Exploration Flight Test-1

2014 unmanned test flight of the Orion spacecraft by NASA From Wikipedia, the free encyclopedia

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 December 5, 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]

NamesOrion Flight Test-1 (OFT-1)
OperatorNASA
Quick facts Names, Mission type ...
Exploration Flight Test-1
Launch of EFT-1 on December 5, 2014
NamesOrion Flight Test-1 (OFT-1)
Mission typeTechnology demonstration
OperatorNASA
COSPAR ID2014-077A Edit this at Wikidata
SATCAT no.40329Edit this on Wikidata
Mission duration4 hours, 24 minutes
Orbits completed2
Spacecraft properties
SpacecraftOrion CM-001
Spacecraft typeOrion
ManufacturerLockheed Martin
Start of mission
Launch dateDecember 5, 2014, 12:05 (2014-12-05UTC12:05Z) UTC (7:05 am EST)[1][2]
RocketDelta IV Heavy
Launch siteCape Canaveral, SLC-37B
ContractorUnited Launch Alliance
End of mission
Recovered byUSS Anchorage
Landing dateDecember 5, 2014, 16:29 (2014-12-05UTC16:30Z) UTC (8:29 am PST)
Landing sitePacific Ocean, 640 mi (1,030 km) SSE of San Diego (23.61°N 114.46°W / 23.61; -114.46 (EFT-1 splashdown))
Orbital parameters
Reference systemGeocentric
Apogee altitude5,800 km (3,604 mi)

Mission insignia
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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.

Objectives

Rendering of Orion capsule and Delta IV upper-stage during EFT-1

EFT-1 tested several systems of the crew module portion of the Orion spacecraft, including separation events, avionics, heat shield performance, parachutes, and recovery operations. The uncrewed test flight served as a precursor to Orion’s first mission aboard the Space Launch System (SLS) on Artemis I. Because the European Service Module was not yet available, Orion flew with a structural representation. It also carried only a partial launch abort system, limited to the motor used to jettison the system at the end of launch, along with an Orion-to-stage adapter designed for future use with the SLS.[5]

For the mission, Orion remained attached to the dummy service module, which itself was connected to the Delta IV Heavy’s upper stage. This stage was nearly identical to the Interim Cryogenic Upper Stage planned for the Block 1 version of the SLS. Unlike future flights, Orion relied on internal batteries for power rather than photovoltaic arrays.[6]

Data returned from EFT-1 informed Orion’s design and were incorporated into its critical design review (CDR) in April 2015.[7] These results helped pave the way for the Artemis I mission, which launched on November 16, 2022,[8] more than seven years after EFT-1.

Vehicle assembly

Orion CM-001 used on the EFT-1 mission was built by Lockheed Martin.[9] On June 22, 2012, the final welds of the EFT-1 Orion were completed at the Michoud Assembly Facility in New Orleans, Louisiana.[9] It was then transported to Kennedy Space Center's Operations and Checkout Building, where the remainder of the spacecraft was completed.[10] The Delta IV rocket was put in a vertical position on October 1, 2014, and Orion was mated with the vehicle on November 11.[11][12][13]

Flight

Mission diagram

The four-and-a-half-hour flight took the Orion spacecraft on two orbits of Earth. Peak apogee was approximately 5,800 kilometres (3,600 mi). The distance allowed the spacecraft to reach reentry speeds of up to 8.9 km/s (20,000 mph), which exposed the heat shield to temperatures up to around 2,200 °C (4,000 °F).[4][5]

More information Time, Event ...
Time Event
L6:00:00Orion powered on, mobile service tower retracts, fueling of Delta IV Heavy begins
0:00:00Launch (7:05 a.m. EST, 12:05 UTC)
0:01:23Max q
0:01:23Vehicle is supersonic
0:03:56Booster separation
0:05:30First stage MECO (main engine cut-off)
0:05:33First stage separation
0:05:49Second stage ignition No. 1
0:06:15Service module fairing jettison
0:06:20Launch Abort System jettison
0:17:39SECO No. 1 (second engine cut-off), Orion begins first orbit
1:55:26Orion completes first orbit, second stage ignition No. 2
2:00:09SECO No. 2
2:05:00Enter first high radiation period
2:20:00Leave first high radiation period
2:40:00Reaction control system (RCS) activation
3:05:00Reach peak apogee: 5,800 km (3,600 mi)
3:23:41Orion separates from combined service module/second stage, second stage performs disposal burn
3:57:00Orion positions for reentry
4:13:41Entry interface
4:20:22Forward bay cover jettisons, parachute deployment begins (two drogues, three mains)
4:24:46Splashdown and recovery by the USS Anchorage crew
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After splashdown in the Pacific Ocean, crews from the USS Anchorage recovered the EFT-1 Orion crew vehicle. Plans were later made to outfit the capsule for an ascent abort test in 2017.[15]

Launch attempts

More information Attempt, Planned ...
AttemptPlannedResultTurnaroundReasonDecision pointWeather go (%)Notes
14 Dec 2014, 7:05:00 amScrubbedWeather4 Dec 2014, 9:44 am (T−00:03:09)A boat entered the launch range, wind gusts in excess of speed limit (21 kn or 24 mph or 39 km/h), and a fuel fill and drain valve did not close. 24-hour recycle.
25 Dec 2014, 7:05:00 amSuccess1 day 0 hours 0 minutes
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Public outreach

NASA heavily promoted the mission, collaborating with Sesame Street and its characters to educate children about the flight test and the Orion spacecraft.[16]

The Orion capsule used for EFT-1 is now on display at the Kennedy Space Center Visitor Complex, in the "NASA Now" exhibit.[17]

References

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