American orbital launch vehicle.
More... - Chronology...
Gross mass: 231,900 kg (511,200 lb).
Height: 38.90 m (127.60 ft).
Diameter: 2.44 m (8.00 ft).
First Launch: 2006.10.26.
Number: 1 .
Stereo American solar satellite. 2 launched, 2006.10.26 (Stereo Ahead) and (Stereo Behind). More...
Delta The Delta launch vehicle was America's longest-lived, most reliable, and lowest-cost space launch vehicle. Development began in 1955 and it continued in service in the 21st Century despite numerous candidate replacements. More...
Associated Manufacturers and Agencies
Douglas American manufacturer of rockets, spacecraft, and rocket engines. Boeing Huntington Beach, Huntington Beach, CA, USA. More...
Associated Launch Sites
Cape Canaveral America's largest launch center, used for all manned launches. Today only six of the 40 launch complexes built here remain in use. Located at or near Cape Canaveral are the Kennedy Space Center on Merritt Island, used by NASA for Saturn V and Space Shuttle launches; Patrick AFB on Cape Canaveral itself, operated the US Department of Defense and handling most other launches; the commercial Spaceport Florida; the air-launched launch vehicle and missile Drop Zone off Mayport, Florida, located at 29.00 N 79.00 W, and an offshore submarine-launched ballistic missile launch area. All of these take advantage of the extensive down-range tracking facilities that once extended from the Cape, through the Caribbean, South Atlantic, and to South Africa and the Indian Ocean. More...
Cape Canaveral LC17B Delta launch complex. Part of a dual launch pad complex built for the Thor ballistic missile program in 1956. Upgraded over the decades for use with Thor, Delta, Delta II, and Delta III launch vehicles, it remained in use for over half a century. More...
Delta Thor XLT-C Lox/Kerosene propellant rocket stage. Loaded/empty mass 101,900/5,900 kg. Thrust 1,054.20 kN. Vacuum specific impulse 302 seconds. More...
Delta K N2O4/Aerozine-50 propellant rocket stage. Loaded/empty mass 6,954/950 kg. Thrust 43.63 kN. Vacuum specific impulse 319 seconds. More...
GEM 40 Solid propellant rocket stage. Loaded/empty mass 13,064/1,361 kg. Thrust 492.93 kN. Vacuum specific impulse 274 seconds. More...
PAM-D Solid propellant rocket stage. Loaded/empty mass 2,141/232 kg. Thrust 67.16 kN. Vacuum specific impulse 292 seconds. More...
PAM-D2 Solid propellant rocket stage. Loaded/empty mass 3,697/431 kg. Thrust 107.20 kN. Vacuum specific impulse 282 seconds. More...
Delta 7925-10L Chronology
2006 October 26 -
00:52 GMT - .
: Cape Canaveral
. Launch Complex
: Cape Canaveral LC17B
. Launch Pad
: SLC17B. LV Family
. Launch Vehicle
: Delta 7925-10L
. LV Configuration
: Delta 7925-10L D319.
- Stereo Ahead - .
Mass: 1,240 kg (2,730 lb). Nation: USA. Agency: Seal Beach. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: Stereo. USAF Sat Cat: 29510 . COSPAR: 2006-047A. The booster was used to put the twin spacecraft in a 182 km x 403,810 km x 28.5 deg lunar transfer orbit. They would use a series of lunar flybys to eventually place themselves in two different solar orbits: Stereo Ahead in a 0.95 AU x 0.97 AU x 0.12
Deg / 344 day orbit around the Sun leading the Earth, and Stereo Behind in a 0.99 AU x 1.09 AU x 0.03 deg / 389 day orbit trailing the Earth. The satellites were equipped with optical, ultraviolet, radio, and particle sensors that would allow them to form a three-dimensional image of the sun's corona using identical sensors from two vantage points at the same moment.
- Stereo Behind - .
Nation: USA. Agency: Seal Beach. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: Stereo. USAF Sat Cat: 29511 . COSPAR: 2006-047B.
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