American all-solid orbital launch vehicle.
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Gross mass: 73,000 kg (160,000 lb).
Height: 31.60 m (103.60 ft).
Diameter: 2.35 m (7.70 ft).
Thrust: 1,380.00 kN (310,230 lbf).
First Launch: 2004.05.20.
Number: 1 .
ROCSAT Taiwanese earth sea satellite. 3 launches, 1999.01.27 (ROCSAT-1) to 2008.10.01 (ROCSAT 2). Taiwan's ROCSAT (Republic of China Satellites) were built for Taiwan's National Space Program Office. More...
Taurus Pad-launched launch vehicle using Pegasus upper stages and Castor-120 first stage. More...
Associated Manufacturers and Agencies
OSC American manufacturer of rockets, spacecraft, and rocket engines. Orbital Sciences Corporation, USA. More...
Associated Launch Sites
Vandenberg Vandenberg Air Force Base is located on the Central Coast of California about 240 km northwest of Los Angeles. It is used for launches of unmanned government and commercial satellites into polar orbit and intercontinental ballistic missile test launches toward the Kwajalein Atoll. More...
Orion 50 Solid propellant rocket stage. Loaded/empty mass 3,370/345 kg. Thrust 118.20 kN. Vacuum specific impulse 292 seconds. More...
Pegasus-3 Solid propellant rocket stage. Loaded/empty mass 985/203 kg. Thrust 34.57 kN. Vacuum specific impulse 293 seconds. More...
SR118 Solid propellant rocket stage. Loaded/empty mass 53,020/4,211 kg. Thrust 1,606.59 kN. Vacuum specific impulse 286 seconds. Modification of Peackeeper ICBM first stage. More...
Taurus-1 Solid propellant rocket stage. Loaded/empty mass 13,242/1,088 kg. Thrust 484.91 kN. Vacuum specific impulse 285 seconds. Pegasus stage 1 without the wings and stabilisers. More...
Taurus 3210 Chronology
2004 May 20 -
17:47 GMT - .
. Launch Complex
: Vandenberg 576E
. LV Family
. Launch Vehicle
: Taurus 3210
. LV Configuration
: Taurus 3210 T7 (XL).
- ROCSAT 2 - .
Payload: LeoStar 500XO. Mass: 760 kg (1,670 lb). Nation: Taiwan. Agency: NSPO. Manufacturer: EADS Astrium. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft: ROCSAT. USAF Sat Cat: 28254 . COSPAR: 2004-018A. Apogee: 891 km (553 mi). Perigee: 887 km (551 mi). Inclination: 99.1000 deg. Period: 102.80 min. Summary: Delayed from October, November 25, 2003; January 17, February 26, April 9 and 22, May 17, 2004..
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