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Aservice module is a component of modular manned spacecraft that may contain life support, power generation, and propulsion systems. Usually unpressurized, the service module remains attached to the pressurized manned capsule during a spaceflight mission and is jettisoned upon the completion of the mission, and usually burns up during atmospheric reentry. The service module is the equivalent to the spacecraft bus assembly on unmanned spacecraft.
After the success of first-generation manned spacecraft in the early 1960s, both the American and Soviet space programs pursued spacecraft supporting more sophisticated mission profiles. In the United States, the early one-man Mercury program was followed by Project Gemini, intended to support two-man crews and longer duration missions. Because of longer duration mission requirements, Gemini required space for equipment and fuel cells instead of batteries for supplying power.[1][2] Gemini featured a manned "re-entry module" (sometimes called the Gemini space capsule) derived and scaled up from the existing Mercury capsule, while adding a separate "adapter module" that contained additional equipment and in-orbit propulsion systems. This increased astronaut safety by keeping consumables (such as fuel for the fuel cells) in a separate module that could be jettisoned shortly prior to re-entry.[1][3]
Depending upon the spacecraft architecture and system design, a typical service module will usually contain the following:[citation needed]
While this would be used for a "baseline" service module, a service module may also be modified for additional functions. An example would be the equipment module on Gemini IX-A, when it was modified to carry the U.S. Air Force-developed Astronaut Maneuvering Unit that would have been tested by astronaut Eugene Cernan, but was cancelled when his spacesuit overheated, causing his visor to fog up. But the best example would be the final three Apollo missions, in which the J-series service modules included scientific instrument module (SIM) bays that took pictures and other readouts in lunar orbit. In addition to the film cameras, similar to those used on the Lunar Orbiter spacecraft and requiring the Command Module Pilot to perform a deep-space EVA during the return trip, two of the SIM bays, on Apollos 15 and 16, also launched a lunar "subsatellite" before the astronauts performed the Trans-Earth Injection burn with the onboard service propulsion system.[citation needed]
A unique inhabitable variation of the service module concept is the Functional Cargo Block developed for the Soviet TKS Transport Supply Spacecraft. In addition to full functionality of a service module, it featured a sizeable pressurized cargo bay, and a docking port - as opposed to its conventional location on the front of the re-entry capsule, which in case of the TKS instead possessed its own downscaled service module with de-orbiting thrusters, allowing the FGB to remain docked as an extension of the space station.
The Russian phrase for service module for the Soyuz spacecraft is sometimes more directly translated "Instrument-Assembly Compartment". This comes from the design feature of having the guidance and other computer systems in a separate pressure chamber (the instruments) from the rocket engines, their propellant tanks, and the life support tanks (from the German Aggregat, which gets translated "assembly"). The Russians use the term "module" (модуль) primarily in regards to elements of a modular space station, e.g. the Zvezda Service Module.
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