Launch of EFT-1 on December 5, 2014 | |
Mission type | Uncrewed test flight |
---|---|
Operator | NASA |
COSPAR ID | 2014-077A |
SATCAT no. | 40329 |
Mission duration | 4 hours, 24 minutes |
Orbits completed | 2 |
Spacecraft properties | |
Spacecraft type | Orion MPCV |
Manufacturer | Lockheed Martin |
Start of mission | |
Launch date | December 5, 2014, 12:05 UTC (07:05 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 | December 5, 2014, 16:29 UTC |
Landing site | Pacific Ocean, 640 miles (1,030 km) SSE of San Diego 23°37′N114°28′W / 23.61°N 114.46°W |
Orbital parameters | |
Reference system | Geocentric |
Apogee | 5,800 kilometres (3,604 mi) |
Orion Program |
Exploration Flight Test 1 or EFT-1 (previously known as Orion Flight Test 1 or OFT-1) was the first test flight of the Orion Multi-Purpose Crew Vehicle. Without a crew, it was launched on December 5, 2014, at 12:05 UTC (7:05 am EST), by a Delta IV Heavy rocket from Space Launch Complex 37B at Cape Canaveral Air Force Station.
The Orion Multi-Purpose Crew Vehicle is an American-European interplanetary spacecraft intended to carry a crew of four astronauts to destinations at or beyond low Earth orbit (LEO). Currently under development by the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA) for launch on the Space Launch System, Orion is intended to facilitate human exploration of the Moon, asteroids and of Mars and to retrieve crew or supplies from the International Space Station if needed.
The Eastern Time Zone (ET) is a time zone encompassing part or all of 22 states in the eastern part of the contiguous United States, parts of eastern Canada, the state of Quintana Roo in Mexico, Panama in Central America, and the Caribbean Islands.
The Delta IV Heavy is an expendable heavy-lift launch vehicle, the largest type of the Delta IV family and the world's second highest-capacity rocket in operation. It is manufactured by United Launch Alliance and was first launched in 2004.
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 20,000 miles per hour (32,000 km/h; 8,900 m/s). [3] This mission design corresponds to the Apollo 4 mission of 1967, which validated the Apollo flight control system and heat shield at re-entry conditions planned for the return from lunar missions.
The term apsis refers to an extreme point in the orbit of an object. It denotes either the points on the orbit, or the respective distance of the bodies. The word comes via Latin from Greek, there denoting a whole orbit, and is cognate with apse. Except for the theoretical possibility of one common circular orbit for two bodies of equal mass at diametral positions, there are two apsides for any elliptic orbit, named with the prefixes peri- and ap-/apo- added to a reference to the body being orbited. All periodic orbits are, according to Newton's Laws of motion, ellipses: either the two individual ellipses of both bodies, with the center of mass of this two-body system at the one common focus of the ellipses, or the orbital ellipses, with one body taken as fixed at one focus, and the other body orbiting this focus. All these ellipses share a straight line, the line of apsides, that contains their major axes, the foci, and the vertices, and thus also the periapsis and the apoapsis. The major axis of the orbital ellipse is the distance of the apsides, when taken as points on the orbit, or their sum, when taken as distances.
Atmospheric entry is the movement of an object from outer space into and through the gases of an atmosphere of a planet, dwarf planet, or natural satellite. There are two main types of atmospheric entry: uncontrolled entry, such as the entry of astronomical objects, space debris, or bolides; and controlled entry of a spacecraft capable of being navigated or following a predetermined course. Technologies and procedures allowing the controlled atmospheric entry, descent, and landing of spacecraft are collectively termed as EDL.
Apollo 4,, was the first unmanned test flight of the Saturn V launch vehicle, which was used by the U.S. Apollo program to send the first astronauts to the Moon. The space vehicle was assembled in the Vertical Assembly Building, and was the first to be launched from Launch Complex 39 at the John F. Kennedy Space Center on Merritt Island, Florida, facilities built specially for the Saturn V.
NASA heavily promoted the mission, collaborating with Sesame Street and its characters to educate children about the flight test and the Orion spacecraft. [4]
The National Aeronautics and Space Administration is an independent agency of the United States Federal Government responsible for the civilian space program, as well as aeronautics and aerospace research.
Sesame Street is an American educational children's television series that combines live action, sketch comedy, animation and puppetry. It is produced by Sesame Workshop and was created by Joan Ganz Cooney and Lloyd Morrisett. The program is known for its images communicated through the use of Jim Henson's Muppets, and includes short films, with humor and cultural references. The series premiered on November 10, 1969, to positive reviews, some controversy, and high viewership; it has aired on the U.S.'s national public television provider PBS since its debut, with its first run moving to premium channel HBO on January 16, 2016.
The flight was intended to test various Orion systems, including separation events, avionics, heat shielding, parachutes, and recovery operations prior to its debut launch aboard the Space Launch System, currently scheduled for some time in 2019. [5]
Avionics are the electronic systems used on aircraft, artificial satellites, and spacecraft. Avionic systems include communications, navigation, the display and management of multiple systems, and the hundreds of systems that are fitted to aircraft to perform individual functions. These can be as simple as a searchlight for a police helicopter or as complicated as the tactical system for an airborne early warning platform. The term avionics is a portmanteau of the words aviation and electronics.
A heat shield is a part of an object designed to protect the object from overheating by dissipating, reflecting or simply absorbing the heat. The term is most often used in reference to exhaust heat management and to systems for dissipation of heat due to friction.
A parachute is a device used to slow the motion of an object through an atmosphere by creating drag. Parachutes are usually made out of light, strong fabric, originally silk, now most commonly nylon. They are typically dome-shaped, but vary, with rectangles, inverted domes, and others found. A variety of loads are attached to parachutes, including people, food, equipment, space capsules, and bombs.
EFT-1 Orion was built by Lockheed Martin. [6] On June 22, 2012, the final welds of the EFT-1 Orion were completed at the Michoud Assembly Facility in New Orleans, Louisiana. [6] It was then transported to Kennedy Space Center's Operations and Checkout Building, where the remainder of the spacecraft was completed. [7] The Delta IV rocket was put in a vertical position on October 1, 2014, and Orion was mated with the vehicle on November 11. [8] [9] [10]
Lockheed Martin Corporation is an American global aerospace, defense, security and advanced technologies company with worldwide interests. It was formed by the merger of Lockheed Corporation with Martin Marietta in March 1995. It is headquartered in North Bethesda, Maryland, in the Washington, DC, area. Lockheed Martin employs approximately 100,000 people worldwide as of December 2017.
The Michoud Assembly Facility (MAF) is an 832-acre (337 ha) manufacturing complex owned by NASA in New Orleans East, a district within New Orleans, Louisiana, in the United States. Organizationally it is part of NASA's Marshall Space Flight Center, and is currently a multi-tenant complex to allow commercial and government contractors, as well as government agencies, to use the site.
The John F. Kennedy Space Center is one of ten National Aeronautics and Space Administration field centers. Since December 1968, Kennedy Space Center has been NASA's primary launch center of human spaceflight. Launch operations for the Apollo, Skylab and Space Shuttle programs were carried out from Kennedy Space Center Launch Complex 39 and managed by KSC. Located on the east coast of Florida, KSC is adjacent to Cape Canaveral Air Force Station (CCAFS). The management of the two entities work very closely together, share resources, and even own facilities on each other's property.
The four-and-a-half-hour flight took the Orion spacecraft on two orbits of Earth. Peak altitude was approximately 5,800 kilometres (3,600 mi). The high altitude allowed the spacecraft to reach reentry speeds of up to 20,000 mph (32,000 km/h; 8,900 m/s), which exposed the heat shield to temperatures up to around 4,000 °F (2,200 °C). [3] [11]
During the flight, the crew module, a structural representation of the service module, a partial launch abort system containing only the jettison motor, and Orion-to-stage adapter were evaluated. [11] The spacecraft remained attached to the Delta IV's upper stage until re-entry began and relied on internal batteries for power rather than photovoltaic arrays, which were not contained in the structural representation. [12] Data gathered from the test flight were analyzed by the critical design review (CDR) in April 2015. [13]
Time | Event |
---|---|
L-6:00:00 | Orion powered on, mobile service tower retracts. Fueling of Delta IV Heavy begins |
0:00:00 | Launch window opens (7:05 a.m. EST, 12:05 UTC). EFT-1 launches. |
0:01:23 | Max Q |
0:01:23 | Reach Mach 1 |
0:03:56 | Booster separation |
0:05:30 | First stage MECO (main engine cut-off) |
0:05:33 | First stage separation |
0:05:49 | Second stage ignition No. 1 |
0:06:15 | Structural representation of service module fairing jettison |
0:06:20 | Launch Abort System jettison |
0:17:39 | SECO No. 1 (second engine cut-off), Orion begins first orbit |
1:55:26 | Orion completes first orbit, second stage ignition No. 2 |
2:00:09 | SECO No. 2 (second engine cut-off) |
2:05:00 | Enter first high radiation period |
2:20:00 | Leave first high radiation period |
2:40:00 | Reaction control system (RCS) activation |
3:05:00 | Reach peak altitude (5,800 kilometers/3,600 miles) |
3:23:41 | Orion separates from service module and second stage, second stage performs disposal burn |
3:57:00 | Orion positions for reentry |
4:13:41 | Entry interface |
4:20:22 | Forward bay cover jettisons, parachute deployment begins (two drogues, three mains) |
4:24:46 | Splashdown |
After splashdown in the Pacific Ocean, crews recovered the EFT-1 Orion crew vehicle and will outfit the capsule for an ascent abort test in 2017. [14]
Attempt | Planned | Result | Turnaround | Reason | Decision point | Weather go (%) | Notes |
---|---|---|---|---|---|---|---|
1 | 4 Dec 2014, 7:05:00 am | Hold | — | Fouled Range | A boat entered the launch range. | ||
2 | 4 Dec 2014, 7:17:00 am | Hold | 0days, 0hours, 12minutes | Weather | Gust wind excess speed limit. (21 knots) | ||
3 | 4 Dec 2014, 7:55:00 am | Hold | 0days, 0hours, 38minutes | Weather | Gust wind excess speed limit. (21 knots) | ||
4 | 4 Dec 2014, 8:26:00 am | Hold | 0days, 0hours, 31minutes | Technical | (T-00:03:09) | A fuel fill and drain valve did not close. | |
5 | 4 Dec 2014, 9:44:00 am | Scrubbed | 0days, 1hour, 18minutes | Technical | 24-hour recycle. | ||
6 | 5 Dec 2014, 7:05:00 am | Success | 0days, 21hours, 21minutes |
Apollo 9 was the third crewed mission in the United States Apollo space program, the second to be sent into orbit by a Saturn V rocket, and the first flight of the command and service module (CSM) with the Apollo Lunar Module. The mission's three-person crew consisted of Commander James McDivitt, Command Module Pilot David Scott, and Lunar Module Pilot Rusty Schweickart. The crew spent ten days in low Earth orbit testing several aspects critical to landing on the Moon, including the LM engines, backpack life support systems, navigation systems, and docking maneuvers.
Gemini 3 was the first crewed mission in NASA's Gemini program. On March 23, 1965, astronauts Gus Grissom and John Young flew three low Earth orbits in their spacecraft, which they nicknamed Molly Brown. This was the ninth crewed US spaceflight, and the 17th world human spaceflight including eight Soviet flights. It was also the final crewed flight controlled from Cape Kennedy Air Force Station in Florida, before mission control functions were shifted to a new control center located at the newly opened Manned Spacecraft Center in Houston, Texas.
The Constellation Program is a cancelled manned spaceflight program developed by NASA, the space agency of the United States, from 2005 to 2009. The major goals of the program were "completion of the International Space Station" and a "return to the Moon no later than 2020" with a crewed flight to the planet Mars as the ultimate goal. The program's logo reflected the three stages of the program: the Earth (ISS), the Moon, and finally Mars—while the Mars goal also found expression in the name given to the program's booster rockets: Ares. The technological aims of the program included the regaining of significant astronaut experience beyond low Earth orbit and the development of technologies necessary to enable sustained human presence on other planetary bodies.
USS Anchorage (LPD-23) is a San Antonio-class amphibious transport dock and the second ship of the United States Navy to be namesake of the U.S. city of Anchorage, Alaska.
Dragon is a reusable cargo spacecraft developed by SpaceX, an American private space transportation company. Dragon is launched into orbit by the company's Falcon 9 two-stage-to-orbit launch vehicle.
The Ares V was the planned cargo launch component of the cancelled NASA Constellation program, which was to have replaced the Space Shuttle after its retirement in 2011. Ares V was also planned to carry supplies for a human presence on Mars. Ares V and the smaller Ares I were named after Ares, the Greek god of war.
A boilerplate spacecraft, also known as a mass simulator, is a nonfunctional craft or payload that is used to test various configurations and basic size, load, and handling characteristics of rocket launch vehicles. It is far less expensive to build multiple, full-scale, non-functional boilerplate spacecraft than it is to develop the full system. In this way, boilerplate spacecraft allow components and aspects of cutting-edge aerospace projects to be tested while detailed contracts for the final project are being negotiated. These tests may be used to develop procedures for mating a spacecraft to its launch vehicle, emergency access and egress, maintenance support activities, and various transportation processes.
Gaganyaan is an Indian crewed orbital spacecraft intended to be the basis of the Indian Human Spaceflight Programme. The spacecraft is being designed to carry three people, and a planned upgraded version will be equipped with rendezvous and docking capability. In its maiden crewed mission, Indian Space Research Organisation's largely autonomous 3.7-tonne capsule will orbit the Earth at 400 km (250 mi) altitude for up to seven days with a three-person crew on board. The crewed vehicle is planned to be launched on ISRO's GSLV Mk III in December 2021. This HAL-manufactured crew module had its first un-crewed experimental flight on 18 December 2014.
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The retirement of NASA's Space Shuttle fleet took place from March to July 2011. Discovery was the first of the three active space shuttles to be retired, completing its final mission on March 9, 2011; Endeavour did so on June 1. The final shuttle mission was completed with the landing of Atlantis on July 21, 2011, closing the 30-year Space Shuttle program.
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