ARCHIVED: Egalotir Space Command

Egalotir

TNPer
OOC: So I'm on winter break so i figured I'd do a fun RP about the Egalotir Space Program. While we have an extensive program i shall start it over to give everyone a view of how things work. I am using Kerbal Space Program as my way of RPing with pictures! For eveyone's sake, the Planet Kerbin is Earth, the little green men are human Egalotirian Astronauts.

Chapter 1: Humble Beginnings

Egalotir has always been one to explore. To drive and push the limits of science. It is on August 23rd, 2006, that the Egalotir Space Command was established with the task of deep space exploration. Along the long term goals, are contracts from various companies that aid budgetary and scientific research wise. To begin, the program began with a simple goal: Build a rocket that can fly, a crew capsule for 1 man, and a communication array to send back data to the Center.

After 4 years under development the Egalotir Space Command(ESC) was constructed:
KSP2014-12-2101-56-11-65.png

It holds a command center, communication array, crew quarters, research laboratories, company contract office, vehicle assembly hanger, spaceplane assembly hangar, and the launch pad. It holds 20,000 active personnel.

Astronaut training began at once, and the top three candidates are as shown:

KSP2014-12-2101-56-22-86.png

Jebediah Kerman: Raised in the capital city of Criovera. Valedictorian at the University of Criovera with a Double Major in Aerospace Engineering and Computer Science with a minor in Mechanical Engineering. Extensive physical and psychological capacity. Top candidate for all missions and head astronaut.

Bill Kerman: Jedediah's younger brother. Equally as capable physically, yet just barely passed the intelligence and psychological screening. He has an adventurous need which can be dangerous, yet equally rewarding. Graduated the University of Dundar with 4.0 GPA with a degree in Aerospace Engineer with a specific concentration in orbital mechanics.

Bob Kerman: No relation to previous astronaut. Undoubtedly the most intelligent of the group, yet the least physically capable. Knowledgeable in Propulsion, Orbital maneuvers, orbital bodies, polymer science, Space Walk(EVA) Specialist. Head Scientist on all missions.

All candidates were required to:
1) have at least a Bachelor's degree from an accredited institution in engineering, biological science, physical science, or mathematics. Degree must be followed by at least three years of related, progressively responsible, professional experience. An advanced degree is desirable and may be substituted for part or all of the experience requirement (master's degree = 1 year of experience, doctoral degree = 3 years of experience). Quality of academic preparation is important.

2) Ability to pass a ESC's space physical, which is similar to a military or civilian flight physical and includes the following specific standards:

Distance visual acuity: 20/200 or better uncorrected, correctable to 20/20, each eye.
Blood pressure: 140/90 measured in a sitting position.
Height between 58.5 and 76 inches.

3) At least 1,000 hours pilot-in-command time in jet aircraft. Flight test experience is highly desirable.


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The current technology tree:

KSP2014-12-2301-44-26-89.png

ESC has spent the last four years researching and testing all areas of aerospace. We have successfully constructed our own crew capsule called the CPC (Crew/Personnel Carrier). It currently only houses 1 crew member and can manually control the spacecraft. Weighs .8 tons and can withstand temperatures of up to 3,400 Kelvin on re-entry. Has an electrical capacity of 50 kV and provides 5 kN*m of torque.

Our Solid Rocket Boosters (SRBs) are composed of the motor (including case, propellant, igniter and nozzle), structure(Aluminum and polymer integration), separation systems, operational flight instrumentation, recovery avionics, pyrotechnics, deceleration system, thrust vector control system and range safety destruct system. Following extensive testings, and numerous failures, our current SRBs have an 88% success rate. It is prone to overheating. Our engineers will continue to improve the numbers. It weighs 3.7475 tons full, .5 tons empty. Has a drag coefficient of .3 and can withstand temperatures of up to 3,900 Kelvins. Provides 250 kN of thrust with a 29 second burn time and 225 Specific Impulse.

The main liquid engine of our program so far is the Daedalus Mk I. Weighs 1.25 tons, 3600 Kelvin max temperature, and provides 215 kN of thrust. This is a Liquid Rocket Engine which uses a liquid oxidizer with a solid or gaseous fuel mix to provide thrust. Our engines use Liquid Oxygen and Liquid Hydrogen. Has a fuel consumption of 13.68 Liters/second. Success Rating: 94%.

The FL-T400 is our main fuel tank. Weighs 2.25 tons, and holds 400 L of fuel, 600 L of Oxidizer.

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After 8 years in development, ECS was ready for it's first flight.
KSP2014-12-2101-57-49-41.png

Egalotir Mk. I sporting one FL-T400, four SRBs, and one CPC. Aboard is Jebediah Kerman, our head astronaut. She stands 27 meters tall on the launch pad:
KSP2014-12-2101-58-04-97.png

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF EGALOTIR I!
KSP2014-12-2101-58-48-24.png

Soaring into clouds, Jebediah relays constant information back to ground command. All is going as planned so far.

Reaching motor burnout, temperatures normal, highest pressure mark passed:

KSP2014-12-2101-58-58-47.png

Reached an apogee of 41,596 meters as well as max speed of 958 m/s. Egalotir I is now on it's way back down to earth, several miles off shore:
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All checks nominal. Prepare for parachute deployment at 700 meters...and....OPEN!

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Finally, a successful splashdown!
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Jebediah reported no errors or issues with the crew capsule. The SRBs and engines were lost on splashdown which was planned. Egalotir Space Command has officially announced this trail a success. Egalotir Mk II is currently being researched and tested for higher atmospheric testing, as well as more efficiency. Our scientists are still shifting through the hundreds of reports of scientific data gathered from the flight.

Next time: Egalotir Mk II.


OOC: What do you guys think? Anything to add or you want to see more of? I will be putting all the updates here and i'll link the next parts in the OP. thanks for reading!

Link to part 2: Egalotir Mk. II:http://forum.thenorthpacific.org/single/?p=8185415&t=7303845
 
OOC: A LOT OF THE SPOILERS HAVE MORE THAN 1 PICTURE


Chapter 2: Egalotir Mk. II:

After a successful first flight, the science team took months to analyze the data from the Egalotir Mk. I post splashdown. First indications showed that the largest deterrent of altitude was weight. A system would need to be developed to separate all spent fuel tanks or SRBs from the launch vehicle. Secondly, the outer atmosphere has very interesting characteristics in terms of pressure and temperature. We should attempt to break the atmosphere at higher speeds. Re-entry of the vehicle was also analyzed to figure out the best flight path for easiest re-entry into the atmosphere.

The resulting technology tree after 2 years in development:
KSP2014-12-2321-42-13-83.png

We have developed a stage separation device called the Separaton Mk. I. It has an ejection impulse of 2,500 Newton-seconds, and only weights .05 tons. It will be used in the Egalotir Mk. II launch for stage separation testing.

We have also developed new sizes of fuel tanks for our liquid fuel engines: FL-T200, and the FL-T100. The FL-T200 is used on the Egalotir Mk. II.

Our very first contract with the company O.M.B. Demolition Enterprises will also be put into effect. They have been tasked with developing an experimental launch pad device to hold the launch vehicle during engine pre-flight fire and releasing for launch:
KSP2014-12-2321-43-32-98.png

The TT18-A Launch Stability Enhancer is going to be tested during the Egalotir Mk. II launch. Three structures will be used to ensure stability of the launch vehicle.

After the ESC has been in service for 10 years, and 6 months, Egalotir Mk. II has been built:
KSP2014-12-2321-46-06-03.png

It holds one FL-T400 tank, one FL-T200 tank and the Daedalus Mk. I liquid fueled engine in the second stage. Two Liquidous Testing Material (LTMs) canisters were also placed to observe the effects of flight on various liquids. The first stage includes the Separaton Mk. I for testing, the TT18-A Launch Stability Enhancer and one SRB.

This flight's goals includes a primary of breaking the atmosphere, with a secondary of semi-orbital flight. Jebediah Kerman will be the one astronaut in this mission, due to his success of the last mission.

Egalotir Mk.II being prepared on the launch pad:
KSP2014-12-2321-46-30-24.png

July 16th, 2016. 10:35 AM.
COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF EGALOTIR II!
KSP2014-12-2321-46-57-41.png
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All checks nominal so far. Approaching stage separation....stage separation initiated...SUCCESS:
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Initiate data collection on LTMs...receiving data:
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Approaching edge of atmosphere...fuel tank 25% remaining:
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Engine burnout comfirmed. First EVA attempt initiated. Jebediah will exit the crew capsule and his flight suit shall collect data on a 30 second long EVA at high altitude. EVA...successful!:
KSP2014-12-2321-48-46-17.png
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Approaching apogee of flight...initiate second stage separation:
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Successful separation. Atmosphere officially broken. Congratulations ECS!
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Initiate second EVA in low altitude space:
KSP2014-12-2321-50-31-84.png

EVA successful, returning to crew capsule. Preparing for re-entry. At this point the vehicle undergoes extreme temperatures and pressures. The flight computer takes over and uses the per-determined flight path calculated by the engineers.

Re-entry underway....temperatures quickly rising.... 600C....700C....800C....900C:
KSP2014-12-2321-51-46-71.png

860C...700C...500C.... Re-entry successful! Connection re-established with the capsule.

Approaching altitude for parachute deployment...OPEN:
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KSP2014-12-2321-52-20-88.png


Splashdown confirmed. Crew capsule and astronaut accounted for. Successful mission all around!
KSP2014-12-2321-53-26-26.png

Post flight report:
Success! We have officially broken the atmosphere of the Earth as well as successful testing of stage separation and ground stability enhancers. Engineers shall begin analysis on the launch vehicle, crew capsule and performance in space as well as all the data collected during flight. Our next mission:

ORBIT!
 
Agreed. This looks like it took a lot of effort. Very interesting read, and I'd like to see where it will go.
 
OOC: Multiple pictures per spoilers.

Chapter3: Testing and Orbit! PART 1

After the successful flight of Egalotir Mk. II, months were spent in the development of experimental technology in terms of SRBs, emergency separation and the new generation of engines. Testing of all systems has been extensive, and the results are shown below:

A new experimental SRB, contracted by the RockoMax Inc., is a huge improvement over currently SRB technology. Standing 50 meters tall, holding twice the fuel of the generation one SRBs with a burn time of 46 seconds. Weighs 7.875 tons full, 1.5 tons empty with a thrust to weight ration of 4.08. Ground tests were conducted by Sidrod Kerman, who has been specially trained on experimental ground testing.

Generation two SRB in assembly hangar:
KSP2014-12-2821-04-13-31.png

On ground test pad:
KSP2014-12-2821-04-38-35.png

RANGE CLEAR....SKIES CLEAR.....GROUND TEST INITIATING....8....7.....6....5....ENGINE FLAME ON...3...2....1...
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A constant 315 kN of thrust was recorded, without incident. tens of SRBs were put to the test, with a current success rate of 74%. Most failures were due to overheating. No personnel have been lost in failure testings. Engineers will continue to improve the SRB until the success rate is adequate for vehicle launch.


RockoMax was also contracted with an emergency separation system. The result of experimentation is the Separatron Mk. I. It is a radially mounted cylinder holding solid rocket fuel, and will ignite in emergency cases. It holds enough thrust(18 kN) to escape main launch vehicle in any desired direction. Testing was supposed to by done by Sidrod Kerman, but he has been relieved on sick leave. Jebediah Kerman was selected as his replacement.

Separatron Mk. I in the assembly hangar:
KSP2014-12-2821-09-29-87.png

RANGE CLEAR....SKIES CLEAR.....GROUND TEST INITIATING....8....7.....6....5....ENGINE FLAME ON...3...2....1...
KSP2014-12-2821-09-48-70.png

Current success rate: 97%. Experimentation stage: Success. Beginning transition into active use.

Lastly, RockoMax's engineers have been working on experimental engines for the second generation of liquid use. It is a radially mounted liquid engine named the Mark 55 Radially Mounted LE. It has 120 kN of thrust, with a thrust to weight ratio of 13.6. It is capable of a 5 degree thrust gimbal(vectoring) and has a high impulse of 320 Ns.

Inside the assembly hangar:
KSP2014-12-2821-07-14-72.png

RANGE CLEAR....SKIES CLEAR.....GROUND TEST INITIATING....8....7.....6....5....ENGINE FLAME ON...3...2....1...
KSP2014-12-2821-07-59-86.png
THRUST LEVEL 40%...SYSTEMS NOMINAL...INCREASING TO 60%...NOMINAL....FULL THRUST:
KSP2014-12-2821-07-48-18.png
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Experimental testing completed and successful. Success rate: 86%. Most failures attributed to failure of ignition or overheating of the nozzle. It is not ready for full vehicle use and more testing will follow.

Our own engineers have also improved our main liquid engine, the Daedalus Mk. I. It is now capable of a 1 degree gimbal thrust vectoring. After extensive testing, Daedalus Mk.II is ready to fly.

Other parts ready for use after extensive testing: TT-38K Radial Decoupler used for decoupling radially mounted SRBs with an ejection force of 2,500 Ns, EAS-4 Strut Connector for increase stability, TVR-1180C Mk1 Stack Tri-Coupler allows for an adaption to three liquid fuel tanks, new radially mounted Mk2 parachutes, aerodynamic radially mounted wings have been created for stability after undergoing wind tunnel tests, and the Aerodynamic Nose Cone which is self explanatory.


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Following the success of Egalotir Mk. II, ECS's next mission was achieving a low earth orbit. Using past technology, newly tested equipment, and the new Daedalus Mk.II, engineers set to work. After 5 months in development, the Criovera Mk. I was ready for launch.

Piloted by Bob Kerman, she stands 145 meters tall. Holds four FL-T400 tanks paired with four new Daedalus Mk.II engines, six radially mounted generation one SRBs connected to the new TT-38K Radial Decouplers. A TVR-1180C Mk1 Stack Tri-Coupler is also used. ThreeAV-T1 Winglets are used as well as the same communication system as previous launches is also used with new Mk2 radially mounted parachutes:
KSP2014-12-2821-14-10-45.png

After the ESC has been in service for 11 years, and 3 months, Criovera Mk. I stands on the launch pad:
KSP2014-12-2821-14-21-99.png

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF CRIOVERA MK.I:
KSP2014-12-2821-14-34-67.png

All systems nominal...increase thrust to 80%. Approaching motor burnout of SRBs...motor burnout complete initiate decoupling...decoupling successful:
KSP2014-12-2821-15-00-12.png

Beginning orbital turn...approaching max pressure stage....and passed...decrease thrust level to 0% and finish turn to 90 degrees...complete. EVA at low earth sub-orbital trajectory... successful:
KSP2014-12-2821-16-07-67.png

Apogee reached...separation of stage...completed. Begin motor burn for orbit:
KSP2014-12-2821-16-45-26.png

Steady...Steady....AND ORBIT ACHIEVED. PERIAPSIS OF 75,000 METERS...APOAPSIS OF 135,000 METERS:
KSP2014-12-2821-17-25-59.png
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Approaching Apoapsis...dark side of the Earth:
KSP2014-12-2821-18-06-20.png

Bob Kerman, the highest Egalotirian astronaut,first to orbit the Earth, first to EVA during Orbit:
KSP2014-12-2821-18-22-29.png

After 2 orbits around Earth, it was time to go home. Begin full thrust burn at 270 degrees at Apoapsis. Burn time: 6 seconds....and cut thrust:
KSP2014-12-2821-20-33-18.png

Begin thrust to decrease orbital speed before re-entry...and motor burnout event reached:
KSP2014-12-2821-21-11-59.png
 
Chapter3: Testing and Orbit! PART 2


Re-entry reached...steady....700C....900C....1200C.....1300C....
KSP2014-12-2821-22-05-89.png
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1200C....1100C....800C...600C....300C... re-entry successful. Prepare for parachute deployment and correction of angle:
KSP2014-12-2821-22-24-50.png

1,500 meters...1,200 meters...900 meters...deploy parachutes....parachutes open!
KSP2014-12-2821-22-34-94.png
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SPLASHDOWN OF THE FIRST EGALOTIRIAN ORBITER: CRIOVERA MK. I, with Bob Kerman:
KSP2014-12-2821-23-49-30.png

Recovery of capsule and astronaut successful.

Next Chapter: More testing, new technology, higher orbits and the future.
 
OOC: This a very long one, 3 parts. Lots of flights! Also I record everything live while i launch things. If something goes wrong, i wont reset i will show failures. Also remember SPOILERS HAVE MORE THAN 1 PICTURE.

Chapter 4: Low-Earth Exploration Part 1

Following a successful orbit of Earth, ESC has received a 35% increase in budget, as well as 5,000 new personnel on base. Data processing began at once, and launch vehicle assembly has been made more efficient. We are now able to construct multiple, readily to launch vehicles in 3 months time.

Current Technology Tree:
KSP2014-12-3021-19-40-02.png

ESC's next priority is to look to the effects of prolong exposure to space flight on the human body as well scientific experiments. In order for a craft to survive for a long period of time in orbit, it must be able to sustain itself with food, water, other supplies, and a readily supply of electricity. Lastly, communication ability has been improved with a new communication dish. The results of testing are new parts used on the Criovera Mk. II:

Z-100 Rechargeable Battery Pack: holds 100kJ of energy to be used per pack and are radially mounted on the craft.
Comms DTS-M1: While consuming 2.5J/second more than the Communitron 16, it has an increase transmitting rate of 6.67 Mits/s opposed to .8 Mits/s of the Communitron 16.
Liquid Observation Canister: Container of various liquids to be observed during prolonged flights and exposure to radiation in outer space.

After 3 months of construction time, the Criovera Mk. II has been unveiled in the Vehicle Assembly Hangar:
KSP2014-12-3021-25-33-69.png

Flown by a new recruit, Derby Kerman, Criovera Mk. II holds 5 Z-100 Batteries, 1 Comms DTS-M1, 1 LOC in the first stage, an FL-T400 with a Daedalus MK.II engine in the second stage, 6 FL-T400s, 6 SRBs generation I, and 3 winglets for aerodynamic support in the last stage for initial launch.

Mission: Prolonged exposure (30 days) to low-earth orbit of 210,000 meters. Data will be recorded constantly throughout flight.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF CRIOVERA MK.II:
KSP2014-12-3021-25-48-48.png
KSP2014-12-3021-25-52-68.png

All systems nominal...approaching SRB motor burnout....motor burnout reached...DECOUPLE:
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Begin gravity turn...hold at 45 degrees:
KSP2014-12-3021-26-45-93.png

Projected apogee reached....begin orbital motor burn:
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Stage II motor burnout achieved...DECOUPLE:
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Continue orbital turn and begin analysis of liquid in low altitude space:
KSP2014-12-3021-28-54-49.png

ORBIT ACHIEVED...CUT THRUST:
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Derby's home for the next 30 days:
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Begin testing of liquids during orbital flight:
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CURRENT ORBITAL TRAJECTORY:
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Begin Day 1 EVA at Apoapsis:
KSP2014-12-3021-32-42-88.png

Report: All systems nominal. Craft has achieved desired orbit, and shall continue to transmit data during flight. All crew reports shall also be posted.

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During the construction of Criovera Mk. II, ESC has also been tasked with learning about the environment around the launch pad as well as how the crafts behave in different environment. All biomes are planned for testing. In order to carry out the testing, a testing platform has been designed and tested, landing legs for the craft have also been extensively tested and a prototype will fly on the Badaloni Mk. I. The new parts are as followed:

LT-1 Landing Struts: First generation of landing struts capable of holding up over 60 tons of weight with a safety factor of 3.0 for the Badaloni Mk.I.
SC-9 Science Testing Module(STM): A testing compartment of various material, all automated during flight. Will be used on all science gathering flights for the purpose of investigating behavior in different biomes. Contains 25Mbits of data.

As a result, three Badaloni Mk. I have been constructed to investigate the highlands biom, behavior in liquidous environments(water) and high altitude testing:
KSP2014-12-3021-36-11-40.png

First stage includes a crew capsule, Mk-16 Parachute, 1 SC-9 STM, and 3 LT-1 Landing Struts. The second stage holds the bulk of the vehicle: 1 FL-T800 fuel tank, 1 Daedalus Mk. II engine,and 4 SRB generation I.

Mission Profile BE-001: Gather data on surrounding highlands around the launch pad as well as test capabilities of the landing struts. Vehicle will be flown by Bill Kerman.

Pre-flight STM check:
KSP2014-12-3021-36-40-95.png

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF Badaloni Mk. I:
KSP2014-12-3021-37-33-70.png

Beginning flight testing of the STM:
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Approaching SRB motor burnout....burnout achieved...DECOUPLE:
KSP2014-12-3021-37-57-55.png
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Part 2 coming up!
 
Chapter 4: Low-Earth Exploration Part 2

Apogee reached...decouple second stage:
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Deploy landing struts and parachute....deployed and all systems check so far:
KSP2014-12-3021-39-51-41.png
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Prepare for landing....500m...400m...300m...200m....100m...50m..20m..:
KSP2014-12-3021-40-18-09.png

Landing successful! The landing struts have proved their worth. All data recorded in the STM during flight has been recovered. Bill has also recovered soil near the landing spot for further analysis:
KSP2014-12-3021-40-58-27.png
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Mission EB-002: Gather scientific data on water landings. Launch Vehicle used: Badaloni Mk.I piloted by Jebediah Kerman.
KSP2014-12-3021-42-39-09.png

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF BADALONI Mk. I:
KSP2014-12-3021-42-55-12.png

SRB motor burnout achieved...DECOUPLE....begin gravity turn:
KSP2014-12-3021-43-38-02.png

Begin counter burn at 270 degrees to achieve straight descent towards Earth:
KSP2014-12-3021-43-59-43.png

Optimal angle achieved...decouple second stage:
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Approaching water landing....deploy parachute and landing struts:
KSP2014-12-3021-44-53-23.png
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100m....50m....30m....20m...:
KSP2014-12-3021-45-36-45.png

Post Flight Analysis: Upon landing, the STM was severely damaged also causing the landing struts to rip off. The capsule was undamaged and the astronaut was recovered, without injury. All data gathered by the STM was also lost on impact.
Conclusion: Avoid water landings at all cost.

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Mission EB-003: STM data gathering of high altitude flight up to 75,000 meters, and a ground landing. Flown by Sidrod Kerman.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF BADALONI Mk.I:
KSP2014-12-3021-46-31-16.png
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SRB motor burnout achieve....DECOUPLE...Full thrust on main engine:
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Begin data gathering from 25,000 meters to apogee...DECOUPLE second stage at main motor burnout:
KSP2014-12-3021-47-39-48.png
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Data Analysis: Very little changed indicated in behavior of materials at high atmospheric altitude.

Prepare deployment of the parachute and landing struts....Deploy!:
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50m....40m...30m....20m...10m...:
KSP2014-12-3021-49-33-13.png

Landing successful, all data and astronaut accounted for.

ESC will continue to construct more Badaloni Mk.I launch vehicles in the coming months to investigate further biomes.

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RockoMax Inc., ESC main contractor, has also been researching and testing new technologies for special cases. The first experimental project is a small scale liquid fuel engine for high-Earth orbital movements and potential docking maneuvers. It uses the same combination of oxidizer and solid fuel as previous engines.

RockoMax 48-7S: Has a max thrust of 30 kN, and a specific impulse of 300 Ns. Due to it's small size, it has a fuel burn rate of .01 kL/s. Finally, it has a gimble capable of a thrust vectoring to 1 degree.

Testing will be performed by test specialist Sidrod Kerman:
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RANGE CLEAR....SKIES CLEAR.....GROUND TEST INITIATING....8....7.....6....5....ENGINE FLAME ON...3...2....1...
KSP2014-12-3021-52-33-88.png
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Chapter 4: Low-Earth Exploration Part 3


INCREASE THRUST TO 65%
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systems nominal...no overheating...FULL THRUST:
KSP2014-12-3021-52-56-27.png

CUT ENGINE THRUST. PREPARE COOLDOWN PROCEDURE.

Testing of the engine has been a success in all trails so far. The engine will be ready for use in the coming months.

RockoMax has also been working on the next line of decouplers for larger sized fuel tanks which are currently in design stage:

RockoMax Brand Decoupler: Weighing .4 tons, this decoupler is designed for larger fuel tanks. It has an ejection impulse of 2,500 Ns.

Testing is conducted by Sidrod Kerman.
KSP2014-12-3021-56-22-99.png


RANGE CLEAR....SKIES CLEAR.....GROUND TEST INITIATING....8....7.....6....5....DECOUPLE SAFETY OFF...3...2....1...
KSP2014-12-3021-56-43-08.png
KSP2014-12-3021-56-47-01.png
KSP2014-12-3021-56-53-71.png

Testing successful as the decoupler was thrown over 45 meters away. All decoupling tests have been successful and this decoupler shall be used when larger vehicles are developed.

---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------

Finally, ESC has finally finished its research involving unmanned flights. The result is an unmanned computer capable of being controlled from the ground station and does not require any astronaut aboard. The very first probe of the Egalotir Space Command has been designed:

Stayputnik Mk. 1: Weights .2 tons, and has a drag coefficient of .15-.2. It can handle a max temperature of 1200K and an impact tolerance of 12 m/s. It has no torque control on any axis and runs completely on electricity consuming 1.67 J/min while only carrying a capacity of 10 kJ. The on board computer is capable of all controls and commands that an astronaut can do. These probes shall be used as satellites to enhance communication with active craft in orbit.

For small thrust control the probe requires, a new small scale engine has also been developed:

LT-50 Liquid Engine: A small scale liquid fuel engine to be used on probes in high Earth orbit. Has a thrust of 50 kN, max temperature of 3,600K a specific impulse of 300 Ns, with a gimble range of .5 degrees. Aftering undergoing excessive testing, with a success rate of 94%, it has been approved for flight.


7 months in development, the Satellite Mk. I has been built:
KSP2014-12-3022-00-45-04.png

First stage holds the unmanned probe, 4 Z-100 Battery Packs, 1 FL-T100 fuel tank, and an LT-50 liquid fuel engine. Second stage is designed for maximum thrust to achieve orbit containing 1 FL-T400 tank with a Daedalus Mk. II engine. Stage three is the main launch vehicle stage containing 1 FL-T800 fuel tank, 1 Daedalus Mk.II engine, and 4 SRBs generation I.

Mission: Achieve a high Earth Orbit of 310,000 meters and successfully communicate with ground command as well as Criovera Mk. II.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF SATELLITE Mk. I:
KSP2014-12-3022-00-57-16.png
KSP2014-12-3022-01-04-33.png

SRB motor burnout achieved...DECOUPLE...begin gravity turn...all systems check:
KSP2014-12-3022-01-35-77.png
KSP2014-12-3022-01-59-71.png

Approaching apogee at 75,000 meters...Decouple second stage...begin orbital reach max thrust:
KSP2014-12-3022-02-22-17.png
KSP2014-12-3022-03-35-32.png

ORBIT ACHIEVED...BEGIN MOTOR BURN OF FT-50 FOR HIGHER ALTITUDE ORBIT....:
KSP2014-12-3022-04-02-67.png

Orbit of 310,000 meters achieved....successful communication with ground...communication with Criovera Mk.II....successful!
KSP2014-12-3022-05-08-81.png
KSP2014-12-3022-06-16-62.png

Mission successful!

Current Flights:
1) Criovera Mk.II at an orbit of 210,000 meters carrying Derby Kerman on a 30 day mission to collect data on long exposure to high Earth altitude and environment.
2) Satellite Mk.I at an orbit of 310,000. Successful communication with all craft and the ground as well as first successful unmanned flight.

Next Chapter: More research...more satellites...
 
You should totally start an RP about this! I'm imagining something like (perhaps) an Egalotir-led joint expedition to, like, Mars or something. Or perhaps a probe intercepting a fictional comet like recently in RL!
 
OOC: multiple pics per spoiler like always. This is a long one haha

Chapter 5: Preparations for the Future Part 1


Egalotir Space Command has seen a lot of success in recent flights and ground tests. After the successful flight of the first Egalotirian Satellite, ESC has allocated majority of funding towards advanced flight controls, automation, and ground testing. The results shall be show below.

Current Technology Tree:
KSP2015-01-0119-58-36-98.png

After undergoing extensive re-design, the RockoMax BACC SRB is ready for further ground testing. This SRB, if successful ground testing occurs, shall be the second generation of SRBs to be used. The SRB stands Standing 50 meters tall, holding twice the fuel of the generation one SRBs with a burn time of 46 seconds. Weighs 7.875 tons full, 1.5 tons empty with a thrust to weight ration of 4.08. Ground tests were conducted by Sidrod Kerman, who has been specially trained on experimental ground testing.

KSP2015-01-0120-03-29-92.png

On the test pad:
KSP2015-01-0120-03-43-28.png

RANGE CLEAR....SKIES CLEAR.....GROUND TEST INITIATING....8....7.....6....5....ENGINE FLAME ON...3...2....1...
KSP2015-01-0120-03-48-31.png
KSP2015-01-0120-03-54-96.png

ENGINE HEAT...NOMINAL...AND ENGINE SHUTOFF ENGAGE:
KSP2015-01-0120-04-36-37.png

Successful testing of BACC SRB is complete. Following more extensive testing, with a success rate of 94%, the SRB generation two has been approved for flight.

ESC's research team has also been designing a new engine specifically for aircraft flight. Prototypes are in design for a first generation of piloted space planes. The team constructed a basic jet engine from design for initial testing. This specific test was a splashdown test to study how the engine would behave when entering water.

A special research launch vehicle was designed to fly from ESC to over the ocean, deploy parachutes, splashdown in the water and begin testing of the engine. The engine is currently named EX-43.

The research vehicle to be piloted by Sidrob Kerman, ESC's test specialist:
KSP2015-01-0120-06-58-91.png

It holds 1 MK.16 parachute, 2 radially mounted MK.2 parachutes, and 3 Daedalus Mk.I with FL-T200 tanks. The X-43 was mounted underneath the pilot capsule.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....LAUNCH:
KSP2015-01-0120-07-15-78.png
KSP2015-01-0120-07-17-69.png

BEGIN OCEAN TURN...BURN TIME 10 SECONDS....ENGINE SHUTOFF
KSP2015-01-0120-07-31-13.png
KSP2015-01-0120-07-34-49.png

APPROACHING LANDING AREA...DEPLOY PARACHUTES
KSP2015-01-0120-07-48-88.png
KSP2015-01-0120-08-05-70.png

STEADY....50m....30m....15m.....SPLASHDOWN. INITIATE ENGINE TESTING AND DATA GATHERING
KSP2015-01-0120-08-40-23.png
KSP2015-01-0120-08-44-53.png

Data gathering and testing has been a success. The engineering team will continue to ground test the engine in the coming months, and make progress towards the first generation of space planes.

Lastly, RockoMax has continued testing on smaller parts designed for future Satellite use. The result is an experimental liquid engine: X24-77. It is a radially mounted engine supplying 20kN of thrust, with a specific impulse of 250 Ns.

Testing conducted by Sidrod Kerman:
KSP2015-01-0120-14-01-77.png

RANGE CLEAR....SKIES CLEAR.....GROUND TEST INITIATING....8....7.....6....5....ENGINE FLAME ON...3...2....1...
KSP2015-01-0120-14-15-57.png

20% THRUST CHECKED....60% THRUST CHECKED...GO TO FULL THRUST....CHECKED
KSP2015-01-0120-14-18-25.png
KSP2015-01-0120-14-21-09.png
KSP2015-01-0120-14-40-37.png

All testings so far have been successful and the engine shall be available for active use in the coming months.

-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------

At the same time, more Badaloni Mk.I have been constructed for further biome data gathering and research. The current bioms planned for research: Highlands and mountain terrain, desert biome, and artic biomes.

Mission Profile BE-003:
The first flight is piloted by a new astronaut, Hantop Kerman, who has been trained in low-earth altitude flights. Landing area are the highlands to the west of ECS.
KSP2015-01-0120-18-55-18.png

First stage includes a crew capsule, Mk-16 Parachute, 1 SC-9 STM, and 3 LT-1 Landing Struts. The second stage holds the bulk of the vehicle: 1 FL-T800 fuel tank, 1 Daedalus Mk. II engine,and 4 SRB generation I.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF Badaloni Mk. I:
KSP2015-01-0120-19-33-55.png
KSP2015-01-0120-19-42-88.png

SRB MOTOR BURNOUT REACHED...DECOUPLE:
KSP2015-01-0120-20-14-35.png


Part 2 Coming up!
 
Chapter 5: Preparations for the Future Part 2


BEGIN SUB-ORBITAL TURN WEST 270 DEGREES....APOGEE REACHED...MOTOR THRUST 100%
KSP2015-01-0120-21-08-13.png
KSP2015-01-0120-21-38-76.png

STAGE 2 MOTOR BURNOUT ACHIEVED...DECOUPLE
KSP2015-01-0120-21-53-37.png

RESEARCH AREA TRAJECTORY ACHIEVED...DEPLOY PARACHUTE...
KSP2015-01-0120-22-18-59.png
KSP2015-01-0120-23-10-17.png

STEADY....100m....50m.....30m....20m....10m....
KSP2015-01-0120-23-30-98.png

Landing successful, begin data collection
KSP2015-01-0120-24-13-88.png

Biome Analysis:
The mountainous region shows that while the ground is solid for landings, it is not desirably flat, along with dirt and rocks being a risk of damaging or contaminating any data or experiments on landing craft. ESC would strongly encourage to avoid highlands landings.

Following the flight, ESC unveiled a new control computer system:

SAS-1: A toggleable module that provides torque and SAS functionality, a sort of autopilot to stabilize and help keep a rocket on course. Extra torque means that the spaceship will rotate faster when ordered to, resulting in a more nimble feel to the craft. The SAS-1 is the entry model reaction wheel. It is cheap, relatively light at .05 tons, with energy consumption of .25J/s. The new computer system will fly on the 4th biome research flight.


Mission Profile BE-003:
Flown by Jebediah Kerman, the Badaloni Mk.I Rev. A will collect data and research on the desert biome far west of ESC. On board the new flight computer is installed, along with a liquid testing capsule.
KSP2015-01-0120-27-10-81.png

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF BADALONI Mk. I REV. A:
KSP2015-01-0120-27-40-42.png
KSP2015-01-0120-27-43-32.png

BEGIN SUB-ORBITAL TURN....SRB MOTOR BURNOUT REACHED....DECOUPLE
KSP2015-01-0120-27-56-94.png
KSP2015-01-0120-28-13-01.png

STAGE 2 MOTOR BURNOUT ACHIEVED...DECOUPLE
KSP2015-01-0120-28-55-21.png

Suddenly ECS realizes that the craft is more than 1,500 km from the research site, with not enough fuel to continue. Mission abort, prepare for water landing.

KSP2015-01-0120-29-45-82.png
KSP2015-01-0120-30-11-35.png
KSP2015-01-0120-30-15-78.png

WE HAVE SPLASHDOWN....CREW ACCOUNTED FOR...RESEARCH MODULE LOST
KSP2015-01-0120-30-38-78.png

Due to calculation errors, the mission had to be aborted due to inadequate amount of fuel to reach research area. An entire re-design of the Badaloni launch vehicle was proposed and promptly approved. 4 months later, the Badaloni Mk.II was ready to be rolled out onto the launch pad.

Mission Profile BE-004B:
Flown by Jebediah Kerman, the Badaloni Mk.I Rev. A will collect data and research on the desert biome far west of ESC using the new Badaloni Mk.II launch vehicle.

KSP2015-01-0120-47-43-05.png


Currently the largest craft in ESC's fleet, it holds 3 stages. Stage 1 is composed of the crew capsule, SAS-1 module, research module, Liquid Testing Capsule, Mk.16 parachute and 3 LT-1 Landing Struts. Stage 2 is composed of the sub-orbital transfer stage of 1 FL-T800 fuel tank, and 1 Daedalus Mk.II. Stage 3 is the main launch vehicle composed of 1 FL-T800 fuel tank, 1 Daedalus Mk.II, 4 generation one SRBs. The launch mechanism has also been re-worked to only include 2 TT18-A Launch Stability Enhancers rather than 4.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF Badaloni Mk. II:
KSP2015-01-0120-47-59-64.png
KSP2015-01-0120-48-05-20.png

SRB MOTOR BURNOUT ACHIEVED...DECOUPLE....STAGE 3 MOTOR BURNOUT ACHIEVED...DECOUPLE
KSP2015-01-0120-49-20-74.png

APOGEE REACHED...BEGIN SUBORBITAL BURN...THRUST 100%
KSP2015-01-0120-50-19-77.png

WE HAVE ACHIEVED RESEARCH AREA LANDING TRAJECTORY...PREPARE TO DECOUPLE STAGE 2
KSP2015-01-0120-50-55-30.png


PART 3 COMING UP
 
Chapter 5: Preparations for the Future Part 3



DECOUPLE STAGE 2...DEPLOY PARACHUTES...
KSP2015-01-0120-51-38-45.png
KSP2015-01-0120-51-43-53.png
KSP2015-01-0120-52-08-30.png

PARACHUTES DEPLOYED...PREPARE FOR DESERT LANDING....50m....40m...20m...10m...
KSP2015-01-0120-52-36-04.png
KSP2015-01-0120-52-54-15.png

INITIATE DATA COLLECTION:
KSP2015-01-0120-53-05-73.png
KSP2015-01-0120-53-14-50.png
KSP2015-01-0120-53-38-17.png

Biome Analysis:
Arid and dry yet landing results in extensive kick-up of dust particles. High level of contamination to research data or experiments on board the craft. Avoid desert landings at all cost.

The final biome to be researched is the arctic north and south poles of Earth. Due to the distance being nearly three times as far as the desert, ESC designed the Badaloni Mk.III. It sports the new generation two SRBs: RockoMax BACC SRBs.

KSP2015-01-0120-54-51-53.png

Mission Profile BE-004:
Land and research the arctic biom to the north of ESC. Piloted by Sidrod Kerman.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
BADALONI Mk. III:
KSP2015-01-0120-55-12-39.png
KSP2015-01-0120-55-43-91.png

SRB BURNOUT ACHIEVED...DECOUPLE...BEGIN SUB-ORBITAL TURN NORTH....STAGE 3 BURNOUT ACHIEVED...DECOUPLE
KSP2015-01-0120-56-02-67.png
KSP2015-01-0120-56-28-38.png

APOGEE REACHED...THRUST 100%
KSP2015-01-0120-57-28-17.png

ARCTIC TRAJECTORY REACHED
KSP2015-01-0120-58-12-07.png

STAGE 2 MOTOR BURNOUT REACHED..DECOUPLE
KSP2015-01-0120-59-12-86.png
KSP2015-01-0120-59-18-16.png

PREPARE FOR LANDING...DEPLOY PARACHUTE
KSP2015-01-0120-59-49-73.png
KSP2015-01-0121-00-16-91.png

50m...40m...30m......20m....10m.....
KSP2015-01-0121-00-41-74.png

INITIATE DATA GATHERING
KSP2015-01-0121-00-52-76.png
KSP2015-01-0121-01-27-33.png

Biome Analysis:
The arctic biome is very cold, which is dangerous for craft vurnable to temperatures as well as critically contaminating and ruining experiments and gathered data. Avoid at all costs.

PART 4 COMING UP
 
Chapter 5: Preparations for the Future Part 4

During development and flights of Badaloni Mk.II and Badaloni Mk.III, there were many improvements in flight control technology and probe technology. New technology research tree:
KSP2015-01-0121-02-13-79.png

ECS's main priority was developing a new probe capable of orbit, in order to increase communication range and efficiency between space objects. Following months of development, the Probodobodyne OKTO is ready for launch. Along with the probe, many advances in electrical and vehicle flight control were also made:

Probodobodyne OKTO: Second generation of probes, it has a simple geometry to allow for more attachments. Weighing .1 tons, with a drag coefficient of .2. Provides a torque of .3 kN per meter, as opposed to 0 by first generation probes. Has an energy storage of 10kJ, and uses 1.2J/min while active.

OX-STAT Photovoltaic Panels: First generation of solar panels to be used during flight. Weighing only .005 tons, they provide a max electrical rate of .75J/s depending on sun exposure.

Z-200 Rechargeable Battery Bank: Second generation of batteries, these are made to mount anywhere on the craft, as opposed to radial mounting. Hold twice the energy(200kJ) of the Z-100 batteries.

Illuminator Mk2: Lighting system for the probes, consumes .2 J/s.

RV-105 RCS Thruster Block: First generation RCS thruster used for spaceship rotation and translation movement and is fueled by mono propellant. This RCS thruster can produce a force in any of the directions its nozzles are pointing. Four of these blocks equally spaced around the body of a vessel is typically enough to allow a small craft to rotate and translate in any direction, but larger ships often require more. Provides 1kN of thrust with an ISP of 100.

Mono propellant:Monopropellant is a resource that is used by RCS thrusters. It is stored in separate tanks from liquid fuel or oxidizer, and may be transferred around a vessel. Stored monopropellant is available to every thruster on a vessel.

The resulting launch vehicle, the Satellite Mk.II:
KSP2015-01-0121-19-11-07.png

Comprised of 3 stages. First stage holds the probe, along with 6 OX-STAT Photovoltaic Panels, 4 Illuminator Mk2, 8 RV-105 RCS Thruster Blocks, 2 Comms DTS-M1, and 1 FL-R25 RCS Fuel Tank holding 250 kg of mono propellant. The second stage is used for orbital burn to achieve orbit using 1 FL-T400 and Daedalus Mk.II. The third stage is the main launch vehicle compromised of 3 FL-T800 with Daedalus Mk.II, and 3 second generation SRBs.

Closeup of the probe:
KSP2015-01-0121-19-16-59.png

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
SATELLITE Mk.II:
KSP2015-01-0121-19-42-82.png

SRB MOTOR BURNOUT COMPLETE...BEGIN 135 DEGREE AXIS TRAJECTORY
KSP2015-01-0121-20-30-02.png

STAGE 3 MOTOR BURNOUT ACHIEVED...DECOUPLE...BEGIN RCS BURN TOWARDS 90 DEGREE Y-AXIS TILT
KSP2015-01-0121-21-09-79.png
KSP2015-01-0121-21-21-81.png

135 DEGREE ORBIT ACHIEVED
KSP2015-01-0121-24-56-57.png

STAGE 2...DECOUPLE
KSP2015-01-0121-25-35-85.png
KSP2015-01-0121-25-52-22.png

Mission success. We have communication with the probe at an orbit of 105,000 meters. Prepare probes 2 and 3 for 315 degree, an 90 degree axis flights.

1 week later:
COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
SATELLITE Mk.II:
KSP2015-01-0121-30-21-44.png

some time later....

ORBIT ACHIEVED AT 315 DEGREE TILT AT 115,000 METERS
KSP2015-01-0121-35-21-17.png

probe 2 flying over the deserts at 2214 meters/second
KSP2015-01-0121-36-33-90.png

Probe 3 orbit achieved at 90 degree tilt at 125,000 meters
KSP2015-01-0121-42-52-57.png

Probe 3 illuminated by the lights on the dark side of Earth
KSP2015-01-0121-43-18-10.png

All probes are actively communicating with the ground, other craft, and each other. We have successfully created an efficient and fast communication system all over Earth.

Current Flights:
1) (MISSION COMPLETED ) Criovera Mk.II at an orbit of 210,000 meters carrying Derby Kerman on a 30 day mission to collect data on long exposure to high Earth altitude and environment.
2) Satellite Mk.I at an orbit of 310,000. Successful communication with all craft and the ground as well as first successful unmanned flight.
3)Satellite Mk.II Probe 1 at an orbit of 105,000
4)Satellite Mk.II Probe 2 at an orbit of 115,000
5)Satellite Mk.II Probe 3 at an orbit of 125,000
 
OOC: Multiple pics per spoiler

Chapter 6: R&D & Preparing For the Moon Part 1

current technology tree:
KSP2015-01-0323-38-00-10.png

To further gather data and research the different biomes around Earth, ECS has designated a mission to set up different research stations for every biome. The launch vehicle took 8 months to design, and is using newly developed technology that allows the external transfer of fuel. This allows the craft to dump dead weight in each of the boosters as soon as fuel is spent. It greatly increases efficiency.

The Biome Research Station Mk.I:
KSP2015-01-0400-16-22-02.png

First stage includes the crew capsule, RCS fuel tank, communication arrays, OX-STAT Photovoltaic Panels for electricity, and a landing mechanism. Second stage involves the high altitude transfer of one FL-T400 tank with a Daedalus Mk.II, and the final 3rd stage includes the new fuel transfer technology. Rather than using SRBs, the craft utilizes external fuel transfers between FL-T800 tanks using Daedalus Mk.II engines, linked to the center FL-T800.

The craft is designed to fly each respective station to the Desert, Arctic, and Highlands.

The first mission, to the desert biome is flown by Aldbur Kerman.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
Research Station Mk.I
KSP2015-01-0400-17-41-39.png
KSP2015-01-0400-18-37-12.png

BOOSTER PAIR I FUEL APPROACHING ZERO....DECOUPLE
KSP2015-01-0400-19-09-56.png

BOOSTER PAIR II FUEL APPROACHING ZERO...DECOUPLE...BEGIN GRAVITY TURN
KSP2015-01-0400-20-00-75.png

APOGEE REACHED...BEGIN GRAVITY BURN
KSP2015-01-0400-21-18-06.png

STAGE III BOOSTER...EMPTY...DECOUPLE
KSP2015-01-0400-21-42-24.png

DESERT TRAJECTORY REACHED...BEGIN COUNTER BURN
KSP2015-01-0400-22-13-07.png
KSP2015-01-0400-23-06-74.png

STAGE II BOOSTER EMPTY...DECOUPLE....DEPLOY PARACHUTES....DEPLOYED
KSP2015-01-0400-23-26-93.png
KSP2015-01-0400-23-44-87.png
KSP2015-01-0400-24-05-31.png

100m..50m.....30m.....20m....10m....
KSP2015-01-0400-24-20-83.png

Successful landing! Deploy communications array...connection with ESC established. Begin data collection.
KSP2015-01-0400-24-56-86.png

Mission 2, flown by Jebediah Kerman, will be stationed in the arctic.


COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
Research Station Mk.I
KSP2015-01-0400-25-38-45.png

small time later....

STAGE II BOOSTER EMPTY...DECOUPLE
KSP2015-01-0400-29-17-22.png

DEPLOY PARACHUTES....
KSP2015-01-0400-30-14-98.png

successful landing! Deploy communications array and begin data collection.
KSP2015-01-0400-31-02-10.png

A third craft has also been launched and successfully landed in the highlands to the west of ESC for data collection.

Part 2: Flashback
 
Chapter 6: R&D & Preparing For the Moon Part 2

Flashback to Derby Kerman months ago:
KSP2015-01-0514-58-02-16.png

Derby Kerman's mission was to survive a 30 day orbit around Earth. The goal of the mission was to collect data on the environment and effects of high altitude orbit conditions for a prolonged period of time. Below is a compilation of the reports sent back by Derby Kerman:

Day 1:

10:46 AM...Here my journey begins. I have enough oxygen, food, electricity, and waste management for 45 days as a precaution. My EVA pack is full, and I am excited for my first step into space....

11:09 AM....I have returned from my very first EVA. It was exhilarating. The suit fully protected me, but I could still feel the coldness of empty space. I examined the capsule upclose as the first task of the EVA, for any possible damage during the ride up here. Everything checks so far.

KSP2015-01-0514-58-36-27.png


Day 7:

5:05 PM...I've been in orbit for a week now. I've rotated Earth about 31 times already. It never gets old, looking down on the planet and just feeling so small. To know that every single living person was beneath me, down there. I was alone up here, 200,000 kilometers away from home, in a tin can, surrounding by emptiness. It's a feeling that I am unable to explain...

Day 18:

8:01 PM... I can feel the effects of lower gravity taking it's toll on my body. I do not feel as strong as I used to, and as a result I have been working out nearly 6 hours a day to gain the same amount of result as back on Earth. When I go back, it's going to be difficult getting used to the changes of being under gravity again. EVAs are the best part of the day though. Earlier today, I completed an extended test of the EVA suit. I flew nearly 3 football fields away from the craft. It was at that point when I felt more alone than I ever had before in my life. There was only a small glass standing between me, and a harsh, cold death. I retreated to the craft shortly after.

KSP2015-01-0514-58-51-03.png

Day 27:

12:01 AM...I've had enough of Astronaut food. I'm ready to go home in three days.

On the 30th day, all systems were checks. Derby Kerman was ready to return home. He began his retrograde burn...
KSP2015-01-0515-01-45-78.png

Re-entry trajectory achieved...decouple second stage
KSP2015-01-0515-02-17-67.png
KSP2015-01-0515-02-40-62.png

Prepare for Re-entry....craft is heating up....600C....700C...800C....700C.....successful re-entry!
KSP2015-01-0515-03-02-63.png

Deploy parachutes!
KSP2015-01-0515-03-51-17.png
KSP2015-01-0515-03-59-42.png


50m...30m....20m....10m.....
KSP2015-01-0515-04-24-30.png

Derby Kerman is home safe!! He will be checked by the medical staff, an data collection will begin at once. This is the first step towards longer missions in orbit.

Part 3: Mun fly by!
 
Chapter 6: R&D & Preparing For the Moon Part 3

Having established a strong research base on Earth, as well as an extensive communications network, ESC was ready to look forward: The Moon. Egalotir is adamant to explore space, and the answers that lie in the cosmos. Egalotir Space Command has a planned 10 year timeline of moon exploration. It begins with a probe flyby to collect data on the gravity field, magnetic field, take pictures of possible landing sites, as well as collect data on how our electronics and equipment behave near, and in orbit with the moon. After a year in development and construction, the MunFlyBy Mk.I was completed.

KSP2015-01-0515-14-16-16.png

It is a 3 stage launch vehicle. The 3rd stage is compromised of six FL-T800 fuel tanks with Daedalus Mk.II engines, and second generation SRBs to help it break out of the Earth's atmosphere. The 2nd stage is an orbital transfer to the moon stage, holding one FL-T400 tank with a Daedalus Mk.II. The 1st stage is compromised of the probe itself, data collection equipment, and solar panels for electricity. It holds one FL-T200 tank with an LV-909 Liquid Fuel Engine to achieve and escape moon orbit. RCS thrusters for control and parachutes for recovery are also in place.

The probe close up:
KSP2015-01-0515-14-33-57.png


A year later, ESC was ready to begin it's journey to the moon.

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
MUNFLYBY Mk.I
KSP2015-01-0515-15-43-75.png

The SRBs have been upgraded with new separation technology to avoid collision with the main launch vehicle as demonstrated below
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GRAVITY TURN COMPLETE....APOGEE REACHED....BEGIN ORBITAL TRANSFER MANEUVER
KSP2015-01-0515-18-32-08.png

3RD STAGE ENGINE BURNOUT...ACHIEVED...DECOUPLE...BEGIN 2ND STAGE BURN
KSP2015-01-0515-18-50-37.png

the moon in view far away
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Orbital transfer achieved!
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Decouple second stage...
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Approaching the moon...Earth behind us
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KSP2015-01-0515-20-42-04.png

BEGIN ORBIT COUNTER BURN.....MOON ORBIT ACHIEVED
KSP2015-01-0515-21-53-73.png

The probe on the low end of the orbit, collecting pictures and data from the moon
KSP2015-01-0515-22-38-01.png

after orbiting for 28 hours and sending data back to ESC, it was time to go home. BEGIN ORBITAL TRANSFER BURN
KSP2015-01-0515-23-20-94.png
KSP2015-01-0515-23-29-07.png
KSP2015-01-0515-24-21-74.png

The dark side of Earth approaching...counter burning to slow down on re-entry
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PREPARE FOR RE-ENTRY
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KSP2015-01-0515-25-53-51.png

DEPLOY PARACHUTES
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50m...40m....30m.....20m...10m...
KSP2015-01-0515-26-55-24.png

We have a successful landing and recovery! Scientists will continue to work on all the data the probe has collected and prepare for the next point in the timeline: landing a probe on the moon!
 
Chapter 6: R&D & Preparing For the Moon Part 4

After the moon flyby, data showed that the connection between ESC and the moon is too weak to transfer larger data sizes. As a result, a new satellite was planned to be put up 3 million kilometers in orbit around the Earth. This heavy satellite will be able to transmit all the data it receives from the moon back to Earth as well as keeping ESC connected. After 8 months, the satellite was launched and successful placed into orbit:

KSP2015-01-0520-10-24-47.png

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Current technology tree:
KSP2015-01-0515-28-38-81.png

Current research stations and satellites:
KSP2015-01-0520-12-01-05.png

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Chapter 6: R&D & Preparing For the Moon Part 5

RockoMax has continued development of specialty engines for outer space missions. The newest design is the Rockomax Mark 55 Radial Mount
Liquid Engine. Unlike conventional engines, this one is radially mounted to the side with fuel connections to the tank. Outputs 120kN of thrust.

The testing required an inflight test of the pump control system. As a result a design vehicle, with an automated computer was designed to fly the engines to around 10,000 meter altitude where testing would take place.

The launch vehicle with four radially mounted Mark 55s:
KSP2015-01-1120-17-54-56.png

On the launch pad:
KSP2015-01-1120-18-22-96.png

COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
MARK 55 TEST VEHICLE
KSP2015-01-1120-19-03-16.png

ALTITUDE REACHED...BEGIN TESTING PROCEDURES
KSP2015-01-1120-19-23-53.png

DEPLOY PARACHUTES...DEPLOYED...PREPARE FOR LANDING
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Landing successful!
KSP2015-01-1120-20-01-85.png

Rockomax deemed the flight a success and the data gathered will help towards putting the engine towards active use.

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At last Egalotir was ready to probe the moon. After 5 years in active research and development, including numerous flybys, the first moon landing launch vehicle has been constructed.

The MunLander Mk.I
KSP2015-01-1221-56-19-10.png

Probe Lander upclose:
KSP2015-01-1221-56-34-53.png

The launch vehicle was compromised of three stage. The first stage is the main launch vehicle for orbital trajectory. It is made up of four 3rd generation SRBs, and one FL-T800 and Daedalus Mk.II engine. The second stage is used for the orbital transfer compromised of one FL-T800 and Daedalus Mk.II engine. The main stage(3rd stage) is the probe lander. Fitted with data collection equipment, along with one FL-T200 and an LV-909 Liquid Fuel Engine for maneuvers. One RCS tank with 4 thrusters are installed to provide extra torque for precision movement, and photoelectric panels for electric collection. An Advanced Inline Stabilizer is also installed to steady the rocket during flight.

MISSION: Achieve moon landing, collect experimental data, achieve re-entry on Earth and recover.

MunLander Mk.I on the pad morning of the launch:
KSP2015-01-1221-57-12-40.png

0736 hours.
COUNTDOWN INITIATED: LAUNCH IN 10....9....8...MAIN ENGINE ON.....7....6.....5....FINAL SEQUENCE CHECK....4....3.....2...1....WE HAVE LAUNCH OF THE
MUNLANDER Mk.I
KSP2015-01-1221-57-18-15.png

ALL SYSTEMS NOMINAL....BEGIN TURN....APPROACHING MAXIMUM AERODYNAMIC PRESSURE...
KSP2015-01-1221-58-19-65.png

SRB MOTOR BURNOUT ACHIEVED...DECOUPLE
KSP2015-01-1221-58-26-00.png

It was later noted that two of the SRBs collided, yet successful splashdown over water was still achieved.

BEGIN SECOND STAGE ORBITAL TRANSFER....
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3RD STAGE MOTOR BURNOUT ACHIEVED...DECOUPLE....BEGIN 2ND STAGE BURN
KSP2015-01-1222-00-19-09.png
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MOON ENCOUNTER ACHIEVED!
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The craft is traveling too fast, begin de-orbital manuever burn at the periapse
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LANDING ENCOUNTER ACHIEVED!

DECOUPLE 2ND STAGE...BEGIN SLOWDOWN BURN
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PREPARE FOR LANDING...DEPLOY LEGS...STEADY...
KSP2015-01-1222-05-25-92.png
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SUCCESS! Egalotir has achieved a moon landing. After countless hours of work, research, trail and error, our first step towards outer space exploration has been achieved.
KSP2015-01-1222-06-09-49.png

Beginning the process of data collection:
KSP2015-01-1222-06-24-70.png
 
Chapter 6: R&D & Preparing For the Moon Part 5 Continued



After spending 19 hours and 4 minutes on the moon, the probe was ready to return back to Earth.
KSP2015-01-1222-06-57-17.png

BEGIN EARTH ORBITAL BURN...ORBIT ACHIEVED....BEGIN EARTH ENCOUNTER BURN...ENCOUNTER ACHIEVED...
KSP2015-01-1222-08-25-29.png

PREPARE FOR RE-ENTRY
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RE-ENTRY ACHIEVED AND SUCCESSFULLY RECOVERED!

A very successful mission, and our analysts will continue to work through the data from the moon. The MunLander Mk.II is being prepared as well with a probe lander upgrade ready to explore more of the moon's surface.
 
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