Names | Orion Flight Test-1 (OFT-1) |
---|---|
Mission type | Technology demonstration |
Operator | NASA |
COSPAR ID | 2014-077A |
SATCAT no. | 40329 |
Mission duration | 4 hours, 24 minutes |
Orbits completed | 2 |
Spacecraft properties | |
Spacecraft | Orion CM-001 |
Spacecraft type | Orion |
Manufacturer | Lockheed Martin |
Start of mission | |
Launch date | 5 December 2014, 12:05UTC (7:05 am EST)[1][2] |
Rocket | Delta IV Heavy |
Launch site | Cape Canaveral, SLC-37B |
Contractor | United Launch Alliance |
End of mission | |
Recovered by | USS Anchorage |
Landing date | 5 December 2014, 16:29UTC (8:29 am PST) |
Landing site | Pacific Ocean, 640 mi (1,030 km) SSE of San Diego (23°37′N 114°28′W / 23.61°N 114.46°W) |
Orbital parameters | |
Reference system | Geocentric |
Apogee altitude | 5,800 km (3,604 mi) |
|
Exploration Flight Test-1 or EFT-1 (previously known as Orion Flight Test 1 or OFT-1) was a technology demonstration mission and the first flight test of the crew module portion of the Orion spacecraft. Without a crew, it was launched on 5 December 2014 at 12:05 UTC (7:05 am EST, local time at the launch site) by a Delta IV Heavy rocket from Space Launch Complex 37B at the Cape Canaveral Air Force Station.[3]
The mission was a four-hour, two-orbit test of the Orion crew module featuring a high apogee on the second orbit and concluding with a high-energy reentry at around 8.9 kilometers per second (20,000 mph).[4] This mission design corresponds to the Apollo 2/3 missions of 1966, which validated the Apollo flight control system and heat shield at re-entry conditions planned for the return from lunar missions.