Difference between revisions of "Tutorial:Salyut programme"
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* 1x [[Mk1-2 Command Pod]] | * 1x [[Mk1-2 Command Pod]] | ||
* 1x [[Communotron 16]] (optional and radial mounted on command pod) | * 1x [[Communotron 16]] (optional and radial mounted on command pod) | ||
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* 1x [[Structural Fuselage]] | * 1x [[Structural Fuselage]] | ||
* 1x [[Communotron 16]] (optional and radial mounted on structural fuselage) | * 1x [[Communotron 16]] (optional and radial mounted on structural fuselage) | ||
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* 4x [[RV-105 RCS Thruster Block]] (radial mounted on RCS tank) | * 4x [[RV-105 RCS Thruster Block]] (radial mounted on RCS tank) | ||
* 2x [[OX-4B Photovoltaic Panels]] (radial mounted on RCS tank) | * 2x [[OX-4B Photovoltaic Panels]] (radial mounted on RCS tank) | ||
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* 2x [[OX-4 Photovoltaic Panels]] (radial mounted on RCS tank) | * 2x [[OX-4 Photovoltaic Panels]] (radial mounted on RCS tank) | ||
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* 1x [[FL-R25 RCS Fuel Tank]] | * 1x [[FL-R25 RCS Fuel Tank]] | ||
* 4x [[RV-105 RCS Thruster Block]] (radial mounted on RCS tank) | * 4x [[RV-105 RCS Thruster Block]] (radial mounted on RCS tank) | ||
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* 2x [[Gigantor XL Solar Array]] (radial mounted on HSC) | * 2x [[Gigantor XL Solar Array]] (radial mounted on HSC) | ||
* 1x [[Rockomax Brand Adapter 02]] | * 1x [[Rockomax Brand Adapter 02]] | ||
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* 1x [[Rockomax Hubmax Multi-Point Connector]] | * 1x [[Rockomax Hubmax Multi-Point Connector]] | ||
− | * 4x [[Clamp- | + | * 4x [[Clamp-O-Tron Docking Port]] |
* 1x [[Rockomax Brand Adapter 02]] | * 1x [[Rockomax Brand Adapter 02]] | ||
* 2x [[PPD-10 Hitchhiker Storage Container]] | * 2x [[PPD-10 Hitchhiker Storage Container]] | ||
* 1x [[Communotron 16]] (radial mounted on HSC) | * 1x [[Communotron 16]] (radial mounted on HSC) | ||
* 3x [[Gigantor XL Solar Array]] (radial mounted on HSC) | * 3x [[Gigantor XL Solar Array]] (radial mounted on HSC) | ||
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====Kvant-1==== | ====Kvant-1==== | ||
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* 1x [[Rockomax Brand Adapter 02]] | * 1x [[Rockomax Brand Adapter 02]] | ||
* 1x [[FL-R1 RCS Fuel Tank]] | * 1x [[FL-R1 RCS Fuel Tank]] |
Revision as of 23:49, 17 June 2013
Welcome to my very first tutorial! Here, we will try to re-enact the world's first space stations. All of the designs are based on actual modules and rockets. Of course, I can't do it perfectly, but I am trying my best. Also, I am doing it without any mod parts.
The Salyut programme was the first space station program undertaken by the Soviet Union, which consisted of a series of four crewed scientific research space stations and two crewed military reconnaissance space stations over a period of 15 years from 1971 to 1986. It was, on the one hand, designed to carry out long-term research into the problems of living in space and a variety of astronomical, biological and Earth-resources experiments, and on the other hand this civilian program was used as a cover for the highly secretive military Almaz stations, which flew as well under the Salyut designation.
Contents
Launcher
Any launcher that can carry a large amount of payload into a low orbit can be used. But I recommend using the Proton-K from the ISS tutorial or any of the launchers from the spacecraft exchange in the KSP forum that could carry at least more than 10 tonnes (I don't know I haven't actually calculated the payloads' weight).
Soyuz personnel transport and Progress unmanned craft
Soyuz is a series of spacecraft initially designed for the Soviet space programme by the Korolyov Space Bureau in the 1960s, and still in service today. The Soyuz succeeded the Voskhod spacecraft and was originally built as part of the Soviet manned lunar programme.
The Progress is a Russian expendable freighter spacecraft. The spacecraft is an unmanned resupply spacecraft during its flight but upon docking with a space station, it allows astronauts inside, hence it is classified manned by the manufacturer. It was derived from the Soyuz spacecraft, and is launched with the Soyuz rocket. It is currently used to supply the International Space Station, but was originally used to supply Soviet space stations for many years. There are three to four flights of the Progress spacecraft to the ISS per year. Each spacecraft remains docked until shortly before the new one, or a Soyuz (which uses the same docking ports) arrives. Then it is filled with waste, disconnected, deorbited, and destroyed in the atmosphere. Because of the different Progress variants used for ISS, NASA uses its own nomenclature where "ISS 1P" means the first Progress spacecraft to ISS.
Ship Design
Front to aft:
- 1x Clamp-O-Tron Docking Port
- 1x Mk1-2 Command Pod
- 1x Communotron 16 (optional and radial mounted on command pod)
- 1x Mk2-R Radial mount parachute (radial mounted on command pod)
- 1x Rockomax Brand Decoupler
- 1x FL-R1 RCS Fuel Tank
- 4x RV-105 RCS Thruster Block
- 2x OX-4B Photovoltaic Panels (radial mounted on RCS tank)
- 1x Rockomax X200-16 Fuel Tank
- 1x Rockomax "Poodle" Liquid Engine
Launch
Try your best to put it on the same orbit as the orbiting Salyut station. If you have an auto-pilot, use the "Launch to rendezvous" function. If not, try to send it with the station.
Rendezvous
Check the tutorials on rendezvous and docking if you don't know how to. The goal is to attach the front end of the Soyuz or Progress to the front end of the station. You may need to switch between vessels to put them in the right directions.
First Generation-The first space stations
Salyut 1
Salyut 1 (DOS-1) was the first space station of any kind, launched by the Soviet Union on April 19, 1971. More stations followed in the Salyut programme, and heritage of that space station program is still in use on the ISS.
Ship Design
Front to aft:
- 1x Clamp-O-Tron Docking Port
- 1x Structural Fuselage
- 1x Communotron 16 (optional and radial mounted on structural fuselage)
- 2x OX-4B Photovoltaic Panels (radial mounted on structural fuselage)
- 1x Rockomax Brand Adapter 02
- 2x PPD-10 Hitchhiker Storage Container
- 1x RC-001S Remote Guidance Unit
- 2x Z-500 Rechargable Battery Bank
- 1x FL-R25 RCS Fuel Tank
- 4x RV-105 RCS Thruster Block (radial mounted on RCS tank)
- 2x OX-4B Photovoltaic Panels (radial mounted on RCS tank)
- 1x Clamp-O-Tron Docking Port
Almaz
The Almaz program was a highly secretive Soviet military space station program, began in the early 1960s.
Three crewed military reconnaissance stations were launched between 1971 and 1974: Salyut 2, Salyut 3 and Salyut 5. To cover the military nature of the program the three launched Almaz stations were designated as civilian Salyut space stations. Salyut 2 failed shortly after achieving orbit, but Salyut 3 and Salyut 5 both conducted successful manned testing. Following Salyut 5, the Soviet Ministry of Defence judged in 1978 that the time consumed by station maintenance outweighed the benefits relative to automatic reconnaissance satellites.
The space stations cores were known internally as OPS, from "Orbital Piloted Station." As part of the Almaz program several spacecraft for supportive roles were developed: The VA spacecraft, the Functional Cargo Block and the TKS spacecraft, which were to be used in several combinations. The heritage of the Almaz program continues to this day with the ISS module Zarya being one example.
Ship Design
Front to aft:
- 1x Clamp-O-Tron Sr. Docking Port
- 2x PPD-10 Hitchhiker Storage Container
- 1x Communotron 16 (radial mounted on HSC)
- 1x Communotron 88-88 (radial mounted on HSC)
- 1x Rockomax Brand Adapter 02
- 2x Z-500 Rechargable Battery Bank
- 1x FL-R25 RCS Fuel Tank
- 4x RV-105 RCS Thruster Block (radial mounted on RCS tank)
- 2x OX-4 Photovoltaic Panels (radial mounted on RCS tank)
- 1x Clamp-O-Tron Docking Port
Salyut 4
Salyut 4 (DOS 4) was a Salyut space station launched on December 26, 1974 into an orbit with an apogee of 355 km, a perigee of 343 km and an orbital inclination of 51.6 degrees. It was essentially a copy of the DOS 3, and unlike its ill-fated sibling it was a complete success. Three crews attempted to make stays aboard Salyut 4 (Soyuz 17 and Soyuz 18 docked; Soyuz 18a suffered a launch abort). The second stay was for 63 days duration, and an unmanned Soyuz capsule remained docked to the station for three months, proving the system's long-term durability. Salyut 4 was deorbited February 2, 1977, and re-entered the Earth's atmosphere on February 3.
Ship Design
Front to aft:
- 1x Clamp-O-Tron Docking Port
- 1x Structural Fuselage
- 1x Communotron 16 (optional and radial mounted on structural fuselage)
- 1x Rockomax Brand Adapter 02
- 2x PPD-10 Hitchhiker Storage Container
- 3x Gigantor XL Solar Array (radial mounted on HSC)
- 1x Rockomax Brand Adapter 02
- 2x Z-500 Rechargable Battery Bank
- 1x FL-R25 RCS Fuel Tank
- 4x RV-105 RCS Thruster Block (radial mounted on RCS tank)
- 1x Clamp-O-Tron Docking Port
Second generation – Long-duration inhabitation of space
In 1977 another marked step forward was made with the second generation of Salyut stations: The aim was to continuously occupy a space station with long-duration expeditions, for the first time in spaceflight.
Although Salyut 6 and Salyut 7 resembled the previous Salyut stations in overall design, several revolutionary changes were made to the stations and program for the aim of continuous occupation: The new stations featured a longer design life and a second docking port at the aft of the stations – crew exchanges and station "hand overs" were now made possible by docking two crewed Soyuz spacecraft at the same time. Furthermore, the uncrewed Progress space station resupply craft was created based on the crewed Soyuz spacecraft, to resupply crew and station with air, air regenerators, water, food, clothing, bedding, mail, propellants, pressurant, and other supplies – while the Progress docked to the station's second docking port, the crew's Soyuz spacecraft could remain docked to the station's first port. The Progress spacecraft can even deliver hardware parts for updating the onboard experiment apparatus and even permitting to perform repairs of the station if needed, furthermore extending the stations life.
The space station program had matured: Flights of both crews and cargo to a space station had become common, and the Salyut stations – first Salyut 6 from 1977 to 1981, and then Salyut 7 from 1982 to 1986 – were crewed continuously for a considerable part of the time.
Salyut 6 and 7
Salyut 6 (DOS-5) was launched on September 29, 1977. Salyut 6 was visited from 1977 until 1981 by 16 manned spacecraft, bringing five long-duration crews ("expeditions") and 11 short-term crews. The very first long-duration crew on Salyut 6 broke a record set on board Skylab, staying 96 days in orbit. The short-term crews included foreign cosmonauts from the Interkosmos programme setting several firsts: the first citizen in space of a nation other than the United States or the Soviet Union, the first black and Hispanic person in space and the first Asian person in space. The longest flight on board Salyut 6 lasted 185 days. The fourth Salyut 6 expedition deployed a 10-meter radio-telescope antenna delivered by an uncrewed cargo spacecraft.
After Salyut 6 manned operations were discontinued in 1981, a heavy unmanned spacecraft called TKS and developed using hardware left from the canceled Almaz program was docked to the station as a hardware test. Some unconfirmed reports say the station was functionally capable of even more missions and years, but combating the ever-increasing mold in living quarters was becoming impossible, and in practice caused the retirement decision. Salyut 6 was deorbited July 29, 1982.
Salyut 7 (DOS-6) was launched on April 19, 1982. DOS-6 was built as the back-up vehicle for Salyut 6 with very similar equipment and capabilities, though several more advanced features were included. The station was aloft for eight years and ten months, during which time it was visited by 10 manned spacecraft bringing six long-duration crews ("expeditions") and 4 short-term crews (including French and Indian cosmonauts in the Interkosmos programme). On 12 February 1985, during an unmanned period, contact with Salyut 7 was lost. The station had became crippled by electrical problems, all systems did shut down and the station began to drift. It was decided to put together a salvage mission, and in June 1985 the Soyuz T-13 mission, in what was in the words of author David S. F. Portree "one of the most impressive feats of in-space repairs in history," managed to bring the station online again. The Soyuz T-15 mission was the last to visit Salyut 7 in 1986, ferrying equipment from Salyut 7 to the new Mir space station; This was so far the only ferry flight between two space stations.
Aside from the many experiments and observations made on Salyut 7, the station also tested the docking and use of large modules with an orbiting space station. These modules, called "Heavy Cosmos modules", helped engineers develop technology necessary to build Mir.
Salyut 7 was finally deorbited on February 7, 1991.
Ship Design
Front to aft:
- 1x Clamp-O-Tron Docking Port
- 1x Structural Fuselage
- 1x Z-500 Rechargable Battery Bank
- 1x FL-R25 RCS Fuel Tank
- 4x RV-105 RCS Thruster Block (radial mounted on RCS tank)
- 1x Communotron 16 (optional and radial mounted on structural fuselage)
- 1x Rockomax Brand Adapter 02
- 2x PPD-10 Hitchhiker Storage Container
- 3x Gigantor XL Solar Array (radial mounted on HSC)
- 1x Rockomax Brand Adapter 02
- 1x Z-500 Rechargable Battery Bank
- 1x Clamp-O-Tron Docking Port
TKS Cosmos Space Module
The TKS spacecraft was a Sovietspacecraft conceived in the late 1960s for resupply flights to the military Almaz space station.
The spacecraft was designed for both crewed or autonomous uncrewed cargo resupply flights, but was never used operationally in its intended role – only four test missions were flown to Salyut space stations during the program. However the Functional Cargo Block (FGB) of the TKS spacecraft would later form the basis of several space station modules, including the Zarya FGB module on the International Space Station.
The TKS spacecraft consisted of two spacecraft mated together, both of which could operate independently: The VA spacecraft (known in the West as the Merkur spacecraft), which would have housed the cosmonauts during launch and reentry of an TKS spacecraft, while traveling to and from an Almaz space station.And the Functional Cargo Block (FGB) which, in order to resupply an Almaz space station, carried docking hardware, tanks and a large pressurized cargo compartment. Furthermore the FGB carried the on-orbit maneuvering engines for the TKS.
While the VA carried the reentry hardware, and only minimal life support and maneuvering systems, the FGB would have been used as the primary orbital maneuvering system and cargo storage for the TKS spacecraft.
The FGB could also be used alone as an unmanned cargo module without an VA spacecraft, which enabled the FGB design to be re-purposed as FGB space station modules later on. The VA spacecraft on the other hand was also intended to be launched as well as "Almaz APOS" mated with an Almaz-OPS space station core, instead of a FGB, as the primary orbital maneuvering system. As of August 2009,Excalibur Almaz planned to use the VA capsule as low-cost cargo return vehicles.
Ship Design
Front to aft:
- 1x Standard NC
- 1x NCS Adapter
- 1x Mk1-2 Command Pod
- 1x Rockomax Brand Decoupler
- 1x FL-R1 RCS Fuel Tank
- 4x RV-105 RCS Thruster Block (radial mounted on RCS tank)
- 1x PPD-10 Hitchhiker Storage Container
- 2x Gigantor XL Solar Array (radial mounted on HSC)
- 1x Rockomax Brand Adapter 02
- 1x Clamp-O-Tron Docking Port
Salyut's heritage – Modular space stations
After the second generation, plans for the next generation of Salyut stations called for the cores DOS-7 and DOS-8 to allow, for the first time in spaceflight, the addition of several modules to a station core and to create a modular space station. For this, the DOS modules were to be equipped with a total of four docking ports: one docking port at the aft of the station as in the second generation Salyuts, and the replacement of the front docking port with a "docking sphere" containing a front, port and starboard docking port.
While the station cores DOS-7 and DOS-8 were build and flown, they never received the Salyut designation; Instead, DOS-7 evolved into the Mir Core Module for the Mir space station that followed the Salyut programme, and DOS-8 was used as the Zvezda Service Module for the International Space Station (ISS) which followed Mir.
And the heritage from the Almaz program is present even today. While in 1976 the last space station from the Almaz programme was flown with Salyut 5, the development of the Almaz TKS spacecraft evolved into the Functional Cargo Block, becoming the first space station modules with the ISS Zarya Functional Cargo Block being in orbit still today.
Mir orbital station
DOS-7 continued to be developed during Salyut 7, becoming the Mir Core Module of the Mir space station – the first modular space station, with crewed operations from 1986 to 2000.
The station featured among others upgraded computers and solar arrays and accommodations for two cosmonauts each having their own cabin. A total of six docking ports were available on the Mir Core Module, which were used for space station modules and visiting spacecraft – the docking sphere design had been upgraded from its initial Salyut design to contain the maximum of five docking ports (front, port, starboard, zenith and nadir). And finally, the modules for the Mir space station were derived from the Functional Cargo Block design of the Almaz programme.
The name of the Mir space station – Russian: Мир, literally Peace or World – was to signify the intentions of the Soviet Union to bring peace to the world; It was however during the time of the Mir space station that the Soviet Union was dissolved in 1991, ending what was began with the 1917October Revolution in Russia. This dissolution had started with the Soviet "perestroika and glasnost" ("restructuring and openness") reform campaigns by Soviet leader Mikhail Gorbachev in the 1980s, had reached an preliminary endpoint with the revolutions of 1989 and the end of the communist Eastern Bloc (Warsaw Pact and the CoMEcon), finally to reach the Soviet Union itself in 1991.
While the Russian Federation became the successor to much of the dissolved Soviet Union and was in a position to continue the Soviet space program with the Russian Federal Space Agency, it faced severe difficulties: imports and exports had steeply declined as the economic exchange with CoMEcon nations had crumbled away, leaving the industry of the former Soviet Union in shambles. Not only did the political change in east-Europe signify an end of contributions to the space program by east-European nations (like from the east-German Carl Zeiss Jena), but parts of the Soviet space industry were located in the newly independent Ukraine, which was similarly cash-strapped as Russia and started to demand hard currency for its contributions.
It was during this time of transition and upheaval that the Shuttle–Mir Program was established between the Russian Federation and the United States in 1993. The former adversaries would now cooperate, with "Phase One" consisting of joint missions and flights of the US Space Shuttle to the Mir space station. It was a partnership with stark contrasts – the Russian needed an inflow of hard currency to keep their space program aloft; In the US it was seen as a chance to learn from the over 20 years of experience of Soviet space station operations, and jumpstart the US space station program.
It was "Phase Two" of this Shuttle-Mir Program that would lead to the International Space Station.
Mir Core Module
Front to aft:
- 1x Clamp-O-Tron Docking Port
- 1x Rockomax Hubmax Multi-Point Connector
- 4x Clamp-O-Tron Docking Port
- 1x Rockomax Brand Adapter 02
- 2x PPD-10 Hitchhiker Storage Container
- 1x Communotron 16 (radial mounted on HSC)
- 3x Gigantor XL Solar Array (radial mounted on HSC)
- 1x Clamp-O-Tron Docking Port
Kvant-1
Front to aft:
- 1x Clamp-O-Tron Docking Port
- 1x Rockomax Brand Adapter 02
- 1x FL-R1 RCS Fuel Tank
- 4x RV-105 RCS Thruster Block (Radial mounted on RCS tank)
- 2x Gigantor XL Solar Array (radial mounted on RCS tank)
- 1x Communotron 16 (Radial mounted on RCS tank)
- 1x Advanced S.A.S Module, Large
- 4x RV-105 RCS Thruster Block (Radial mounted on SAS module)
The Original Missions
The original Salyut space stations were in orbit in 1971-1986.The first space station was Salyut 1, which was launched by the Soviet Union on April 19, 1971. Like all the early space stations, it was "monolithic", intended to be constructed and launched in one piece, and then manned by a crew later. As such, monolithic stations generally contained all their supplies and experimental equipment when launched, and were considered "expended", and then abandoned, when these were used up.
The second generation of salyut stations were in orbit in 1986-present day. Plans for the stations called for the cores to allow, for the first time in spaceflight, the addition of several modules to a station core and to create a modular space station.For this, the DOS modules were to be equipped with a total of four docking ports: one docking port at the aft of the station as in the second generation Salyuts, and the replacement of the front docking port with a "docking sphere" containing a front, port and starboard docking port.While the station cores DOS-7 and DOS-8 were build and flown, they never received the Salyut designation; Instead, DOS-7 evolved into the Mir Core Module for the Mir space station that followed the Salyut programme, and DOS-8 was used as the Zvezda Service Module for the International Space Station (ISS) which followed Mir.
The modules was placed on a Low Earth Orbit, which usually corresponds to 160 to 2000 km. So, if you want to make it good, launch as usual, with a gravity turn starting at 10km. Continue until you reach a low apoapsis, then burn there to get a low periapsis a few kilometres from the height of your apoapsis and get an almost circular orbit. It is very possible to achieve this orbit with precise flying.
What now
You could do the International Space Station and/or possibly your own space station, interplanetary base, etc. let your imagination run wild!