American manufacturer of spacecraft. Massachusetts Institute of Technology, USA.
More... - Chronology...
Hunsaker Hunsaker, Jerome C (1886-1984) American engineer. Organized and headed department of aeronautical engineering at MIT, 1939-1951. Influentical, and discouraged development of jet and rocket propulsion in the US before 1945. More...
Chapman Chapman, Philip Kenyon (1935-) Australian scientist astronaut, 1967-1972. More...
Young, Lawrence Young, Lawrence Retman (1935-) American engineer payload specialist astronaut, 1991-1993. More...
Lichtenberg Lichtenberg, Dr Byron Kurt (1948-) American engineer payload specialist astronaut. Flew on STS-9, STS-45. Flew 138 combat missions in Vietnam. More...
Mars Cycler American manned Mars flyby. Study 1989. As part of a space infrastructure, it was proposed that four space stations be placed in cyclical orbits. These would allow departures for a six-month journey to Mars every 26 months. More...
HETE American gamma ray astronomy satellite. 2 launches, 1996.11.04 (HETE) and 2000.10.09 (HETE-2). The High Energy Transient Experiment (HETE) was an international mission led by The Massachusetts Institute of Technology (MIT). More...
Bio-Suit American space suit, study of 2001. Novel approach that used biomedical breakthroughs in skin replacement and materials to replace the bulky conventional balloon spacesuit with a second skin approach. More...
2000 October 9 -
05:38 GMT - .
: Kwajalein DZ
. Launch Pad
: 7.7 N x 167.7 E. Launch Platform
: L-1011. LV Family
. Launch Vehicle
: Pegasus H
. LV Configuration
: Pegasus H F30/P-35.
- HETE-2 - .
Mass: 130 kg (280 lb). Nation: USA. Agency: NASA Greenbelt. Manufacturer: MIT. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: HETE. USAF Sat Cat: 26561 . COSPAR: 2000-061A. Apogee: 641 km (399 mi). Perigee: 598 km (372 mi). Inclination: 1.9497 deg. Period: 97.02 min. First orbital launch from Kwajalein. Second High Energy Transient Explorer; built by MIT using leftover parts from the first HETE. This failed to operate because of a Pegasus adapter failure during launch in November 1996. MIT operates the satellite, while the program is managed by NASA GSFC as an Explorer mission of opportunity. HETE's main instrument is FREGATE, the French Gamma Telescope, a hard X-ray spectrometer operating in the 6 to 400 keV energy range. This gamma ray burst detector, together with a Wide Field X-ray Monitor hard X-ray coded mask telescope, is used to trigger searches with the two Soft X-ray Imagers which have 33-arcsecond spatial resolution. This will let astronomers get precise locations for gamma-ray bursts, allowing detailed follow-up with optical instruments. The satellite is in a 595 x 636 km x 2.0 deg equatorial orbit, and sends data to a network of small ground terminals spaced around the equator.
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