Lockheed Martin Orion MPCV 2014 - Hero viewLockheed Martin Orion MPCV 2014 - Top View viewLockheed Martin Orion MPCV 2014 - Profile viewLockheed Martin Orion MPCV 2014 - Bottom View viewLockheed Martin Orion MPCV 2014 - Cockpit viewLockheed Martin Orion MPCV 2014 - Flight Displays viewLockheed Martin Orion MPCV 2014 - Hatch viewLockheed Martin Orion MPCV 2014 - Stowage viewLockheed Martin Orion MPCV 2014 - Docking System viewLockheed Martin Orion MPCV 2014 - Engine viewLockheed Martin Orion MPCV 2014 - Heat Shield viewLockheed Martin Orion MPCV 2014 - Solar Array view
Hero
Still operational

NASA''s deep-space crew vehicle for the Artemis Moon program. Orion flew farther from Earth than any spacecraft designed for humans when it traveled 268,563 miles during Artemis I. It is the only active vehicle designed to return crews from lunar distances.

History

Orion has its roots in the Crew Exploration Vehicle concept from NASA''s Constellation program, first proposed in 2004 as part of the Vision for Space Exploration. When Constellation was cancelled in 2010, Orion survived as the Multi-Purpose Crew Vehicle, retained by Congress for deep-space missions.

The capsule is significantly larger than Apollo''s Command Module, designed to carry four astronauts for missions lasting up to 21 days. Its heat shield, the largest ever built for a human-rated spacecraft, must withstand reentry speeds of 25,000 mph when returning from the Moon -- far more severe than returns from low Earth orbit.

Orion completed its first test flight (EFT-1) in December 2014 aboard a Delta IV Heavy, reaching an altitude of 3,604 miles. The Artemis I mission in late 2022 was the first flight of the complete SLS/Orion system, sending an uncrewed Orion around the Moon. The Artemis II mission will carry four astronauts on a similar trajectory, making them the first humans to travel beyond low Earth orbit since Apollo 17 in 1972.

Timeline

2004First proposed in 2004 as part of the Vision for Space Exploration
2010When Constellation was cancelled in 2010
2014First flight
2022The Artemis I mission in late 2022 was the first flight of the complete SLS/Orion system

Launch Heritage

Operational StatusOperational
Total Launches2/2 (100%)
Service Period2014
DesignerLockheed Martin / NASA
Mission Typecrewed_orbital
ReusabilityExpendable
Orbit Typelunar
Target BodyMoon
Notable Missions
  • EFT-1
  • Artemis I

Technical Specifications

PropulsionHypergolic
Height16.4 ft
Length16.4 ft
Diameter/Wingspan16.5 ft
Crew4
Gross Mass58,467 lbs
Empty Mass22,928 lbs

Propulsion

Engine ModelAJ10-190 (OMS-E)
Engine Count1
Engine ManufacturerAerojet Rocketdyne
Thrust33.4 kN
Specific Impulse316 s
PropellantMMH/N2O4 (Hypergolic)

Dimensions

Height (m)5 m
Diameter (m)5.02 m
Length (m)5 m

Mass

Empty Mass (kg)10,400 kg
Gross Mass (kg)26,520 kg

Mission

Crew Capacity4
Mission Duration21 days (max)
Missions Flown2
Success Rate2/2
ReusableYes

Power & Systems

Power Output11,200 W
Solar Array Area75 m²
Battery TypeSolar arrays + Li-ion batteries
AvionicsHoneywell RHEL flight computers, Orion GN&C, ESA service module avionics
Communication BandS-band, Ka-band via TDRSS + DSN for lunar distance

Tags

Designed by Lockheed Martin / NASA

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