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Delta 7320-10C
Part of Thor
American orbital launch vehicle. 3 stage vehicle consisting of 3 x GEM-40 + 1 x EELT Thor + 1 x Delta/0020.
AKA: Delta 7320-XC. Status: Active. First Launch: 2004-11-20. Last Launch: 2015-01-31. Number: 8 . Gross mass: 151,700 kg (334,400 lb). Height: 38.90 m (127.60 ft). Diameter: 2.44 m (8.00 ft).
More at: Delta 7320-10C.
Family:
orbital launch vehicle.
Country:
USA.
Spacecraft:
LEOStar-2,
Proteus,
SAC-D,
SMAP,
TIROS,
Advanced Tiros N,
Cubesat,
Swift,
RS-300.
Launch Sites:
Cape Canaveral,
Vandenberg,
Cape Canaveral LC17A,
Vandenberg SLC2W.
Stages:
Delta Thor XLT-C,
Delta K,
GEM 40.
Agency:
Douglas.
2004 November 20 - .
17:16 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17A.
Launch Pad: SLC17A.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- Swift - .
Payload: SA-200LL. Mass: 1,331 kg (2,934 lb). Nation: USA.
Agency: NASA.
Manufacturer: Gilbert.
Class: Astronomy.
Type: Gamma ray astronomy satellite. Spacecraft Bus: SA-200.
Spacecraft: Swift.
USAF Sat Cat: 28485 . COSPAR: 2004-047A. Apogee: 604 km (375 mi). Perigee: 584 km (362 mi). Inclination: 20.60 deg. Period: 96.60 min. NASA Medium-class Explorer satellite dedicated to study of gamma ray bursts, the third after the IMAGE and WMAP satellites. Delayed from December 5 and 29, 2003, January 14, April 29, July 15, September 1, October 7 and 26, November 8, 11, 17, 18 and 19..
2005 May 20 - .
10:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- NOAA 18 - .
Payload: NOAA-N. Mass: 1,420 kg (3,130 lb). Nation: USA.
Agency: NOAA.
Manufacturer: Lockheed.
Program: Tiros.
Class: Earth.
Type: Weather satellite. Spacecraft: Advanced Tiros N.
USAF Sat Cat: 28654 . COSPAR: 2005-018A. Apogee: 866 km (538 mi). Perigee: 847 km (526 mi). Inclination: 98.70 deg. Period: 102.10 min. Delayed from June 30, 2004, February 12, March 10 and 19, May 11, 12, 13 and 14..
2008 June 20 - .
07:46 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- Jason 2 - .
Mass: 506 kg (1,115 lb). Nation: France.
Agency: Martin.
Class: Earth.
Type: Earth resources satellite. Spacecraft: Proteus.
USAF Sat Cat: 33105 . COSPAR: 2008-032A. Apogee: 1,344 km (835 mi). Perigee: 1,332 km (827 mi). Inclination: 66.00 deg. Period: 112.40 min. Ocean Surface Topography Mission follow-on to Jason 1. Carried Poseidon-3 altimeter for precision measurement of ocean surface and the NASA Advanced Microwave Radiometer to measure atmospheric moisture in the path of the altimeter beam..
2009 February 6 - .
10:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- NOAA 19 - .
Payload: NOAA-O. Mass: 1,420 kg (3,130 lb). Nation: USA.
Agency: NOAA.
Manufacturer: Lockheed.
Program: Tiros.
Class: Earth.
Type: Weather satellite. Spacecraft: Advanced Tiros N.
USAF Sat Cat: 33591 . COSPAR: 2009-005A. Apogee: 867 km (538 mi). Perigee: 845 km (525 mi). Inclination: 98.80 deg. Period: 102.10 min.
2009 December 14 - .
14:09 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- WISE - .
Mass: 674 kg (1,485 lb). Nation: USA.
Agency: Martin.
Class: Astronomy.
Type: Infrared astronomy satellite. Spacecraft: RS-300.
USAF Sat Cat: 36119 . COSPAR: 2009-071A. Apogee: 532 km (330 mi). Perigee: 527 km (327 mi). Inclination: 97.50 deg. Period: 95.20 min.
Wide Field Infrared Explorer astronomy satellite, designed to conduct an all-sky survey at infrared frequencies of 3.4, 4.6, 12 and 22 microns, detecting objects 100 times fainter than the earlier IRAS and Akari satellites. Primary instrument is a 40 cm telescope cooled to 12 K by a cryostat filled with solid hydrogen. The survey was expected to detect tens of thousands of new asteroids, brown dwarf stars, and planets orbiting nearby stars.
2011 June 10 - .
14:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
2014 July 2 - .
09:56 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- OCO 2 - .
Mass: 407 kg (897 lb). Nation: USA.
Spacecraft: Leostar-2.
USAF Sat Cat: 40059 . COSPAR: 2014-035A. Apogee: 704 km (437 mi). Perigee: 701 km (435 mi). Inclination: 98.20 deg. Period: 98.83 min. Was to have provided space-based observation of atmospheric carbon dioxide..
2015 January 31 - .
14:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- FIREBIRD IIA - .
Mass: 2.00 kg (4.40 lb). Nation: USA.
Class: Science.
Type: Space science. Spacecraft: Cubesat.
USAF Sat Cat: 40377 . COSPAR: 2015-003B. Apogee: 643 km (399 mi). Perigee: 431 km (267 mi). Inclination: 99.10 deg. Period: 95.38 min. 1.5U cubesat by NSF/Montana State/U. New Hampshire space science satellite. Sun synchronous orbit; 0600 GMT local time of the descending node..
- FIREBIRD IIB - .
Mass: 2.00 kg (4.40 lb). Nation: USA.
Class: Science.
Type: Space science. Spacecraft: Cubesat.
USAF Sat Cat: 40378 . COSPAR: 2015-003C. Apogee: 643 km (399 mi). Perigee: 431 km (267 mi). Inclination: 99.10 deg. Period: 95.38 min. 1.5U cubesat by NSF/Montana State/U. New Hampshire space science satellite. Sun synchronous orbit; 0600 GMT local time of the descending node..
- GRIFEX - .
Mass: 4.00 kg (8.80 lb). Nation: USA.
Class: Technology.
Type: Technology satellite. Spacecraft: Cubesat.
USAF Sat Cat: 40379 . COSPAR: 2015-003D. Apogee: 648 km (402 mi). Perigee: 433 km (269 mi). Inclination: 99.10 deg. Period: 95.45 min. 3U cubesat by Michigan/JPL; technology satellite. Sun synchronous orbit; 0600 GMT local time of the descending node..
- ExoCube CP10 - .
Mass: 4.00 kg (8.80 lb). Nation: USA.
Class: Earth.
Type: Atmosphere satellite. Spacecraft: Cubesat.
USAF Sat Cat: 40380 . COSPAR: 2015-003E. Apogee: 652 km (405 mi). Perigee: 434 km (269 mi). Inclination: 99.10 deg. Period: 95.51 min. 3U cubesat by California Polytechnic. Sun synchronous orbit; 0600 GMT local time of the descending node..
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