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Delta 7920H
Part of Thor
Delta 7000H Credit: © Mark Wade |
American orbital launch vehicle. Version of Delta 7000 using much larger GEM 46 solid rocket motors originally developed for the Delta 3.
Status: Active. First Launch: 2003-08-25. Last Launch: 2011-09-10. Number: 3 . Payload: 1,816 kg (4,003 lb). Thrust: 4,510.00 kN (1,013,880 lbf). Gross mass: 286,000 kg (630,000 lb). Height: 39.00 m (127.00 ft). Diameter: 2.44 m (8.00 ft).
LEO Payload: 1,816 kg (4,003 lb). Payload: 1,000 kg (2,200 lb) to a earth escape.
More at: Delta 7920H.
Family:
orbital launch vehicle.
Country:
USA.
Spacecraft:
LM-300,
SA-200,
MER,
SIRTF,
GLAST.
Launch Sites:
Cape Canaveral,
Cape Canaveral LC17B.
Stages:
Delta Thor XLT-C,
Delta K,
GEM 46,
Star 48.
Agency:
Douglas.
2003 August 25 - .
05:35 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
Launch Pad: SLC17B.
LV Family:
Thor.
Launch Vehicle:
Delta 7920H.
- SIRTF - .
Mass: 923 kg (2,034 lb). Nation: USA.
Agency: NASA.
Class: Astronomy.
Type: Infrared astronomy satellite. Spacecraft: SIRTF.
USAF Sat Cat: 27871 . COSPAR: 2003-038A.
Originally to have launched January 9, 2003. Delayed six times. The Space Infrared Telescope Facility (SIRTF) was the last of NASA's 'Great Observatories'. It had a 0.85-meter infrared telescope, with a liquid-helium cooled focal plane carrying the three main instruments. SIRTF was launched by the second Delta II Heavy. The second stage entered a 166 x 167 km x 31.5 deg Earth parking orbit, and after about 33 minutes of coast, passing south of Madagascar, restarted at 0613 UTC to enter a hyperbolic orbit with a perigee of 170 km, an eccentricity of 1.0061, and a velocity of 11.05 km/s. This placed it in a solar orbit of 0.996 x 1.019 AU x 1.14 deg with a year about 4 days longer than Earth's.
2008 June 11 - .
16:05 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
Launch Pad: SLC17B.
LV Family:
Thor.
Launch Vehicle:
Delta 7920H.
- Fermi Gamma Ray Space Telescope - .
Payload: SA-200HP. Mass: 500 kg (1,100 lb). Nation: USA.
Agency: Martin.
Class: Astronomy.
Type: Gamma ray astronomy satellite. Spacecraft: SA-200.
USAF Sat Cat: 33053 . COSPAR: 2008-029A. Apogee: 562 km (349 mi). Perigee: 542 km (336 mi). Inclination: 25.60 deg. Period: 95.70 min. Gamma-ray Large Area Space Telescope; renamed Fermi GST after launch..
2011 September 10 - .
13:08 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
Launch Pad: SLC17B.
LV Family:
Thor.
Launch Vehicle:
Delta 7920H.
- Grail A Ebb - .
Mass: 202 kg (445 lb). Nation: USA.
Class: Moon.
Type: Lunar probe. Spacecraft: LM-300.
Decay Date: 2012-12-17 . USAF Sat Cat: 37801 . COSPAR: 2011-046A.
NASA dual-spacecraft lunar gravity mapping mission. Grail A was deployed from the Delta upper stage at 14:28 GMT and Grail B at 14:37 GMT. The spacecraft reached the Sun-Earth L1 point 1.5 million km from Earth and then fell back towards the Moon. Lunar orbit insertion was at 01:00 GMt on 1 January 2012 for Grail A, and at 02:00 GMT on 2 January for Grail B. After completing their mission, the satellites were intentionally crashed onto the lunar surface at 75.62 deg N / 26.63 deg W on 17 December 2012 at 22:29 GMT.
- Grail B Flow - .
Mass: 202 kg (445 lb). Nation: USA.
Class: Moon.
Type: Lunar probe. Spacecraft: LM-300.
Decay Date: 2012-12-17 . USAF Sat Cat: 37802 . COSPAR: 2011-046B.
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