Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

Orion (MPCV)

Orion-MPCV [ESA]

Orion MPCV (Multi-Purpose Crew Vehicle) is planned manned spacecraft for missions to the moon, asteroids and eventually to Mars.

MPCV ia a capsule design, which inherits its shape from the Apollo capsule, but is otherwise a completly new construction. It was to launched on a Ares-1 launcher derived from Space Shuttle technology. In contrast to Apollo, landing will be on land, assisted by air-bags or retro-rockets.

After the Constellation was cancelled, the Orion CEV capsule was renamed Orion Multi-Purpose Crew Vehicle (MPCV). It will serve as a vehicle for lunar and interplanetary missions. The LEO missions to ISS will instead be flown on commercial vehicles.

An unmanned testflight of a Orion capsule without service module called Orion-EFT 1 launched by a Delta-4H rocket was launched in December 2014.

In late 2012 ESA joined the project and will provide a service module for Orion based on the ATV service module. The OME main engine for the first three missions are Aerojet AJ10-190 (OMS) engines left over from the Shuttle. Later missions will feature a different engine, possibly with green propellants.

The first Orion MPCV capsule, the uncrewed EM-1 mission, will be launched in 2020 on a SLS (Block 1) rocket. In March 2019 NASA announced, that they are considering launching the EM-1 missions on two commercial launch vehicles (Falcon-Heavy (Block 5)) instead, with one launcher orbiting the Orion capsule and the other the transfer stage.

The second will follow in 2022 on a SLS (Block 1) iCPS rocket on a mission to lunar orbit, carrying four astronauts.

Later, Orion MPCV will perform lunar and interplanetary missions using the improved SLS (Block 1B) EUS launch vehicle.

Nation: USA
Type / Application: Manned spacecraft
Operator: NASA, ESA
Contractors: Lockheed Martin (prime, capsule); EADS Astrium → Airbus Defence and Space (service module)
Propulsion: OME (AJ10-190), 8 × R-4D-11-300
Power: 4 deployable solar arrays, batteries
Lifetime: 180 days
Mass: 25848 kg (total); 10387 kg (capsule); 15461 kg (service modulke)
Satellite COSPAR Date LS Launch Vehicle Remarks
Orion Artemis-1 (EM-1) - 2020 CCK LC-39B SLS (Block 1) iCPS with BioSentinel, CuSP, LunaH-Map, Lunar-Flashlight, Lunar-IceCube, NEA-Scout, LunIR, EQUULEUS, OMOTENASHI, ArgoMoon, Cislunar Explorer A, Cislunar Explorer B, CU-E3, Miles
Orion Artemis-2 (EM-2) - 2023 CCK LC-39B SLS (Block 1) iCPS
Further Orion (CEV) missions: