American all-solid orbital launch vehicle. Four stage vehicle consisting of 1 x Algol 2A + 1 x Castor + 1 x Antares 2 + 1 x MG-18
Gross mass: 17,000 kg (37,000 lb).
More... - Chronology...
Height: 22.00 m (72.00 ft).
Diameter: 1.02 m (3.34 ft).
Thrust: 380.00 kN (85,420 lbf).
Apogee: 900 km (550 mi).
First Launch: 1963.02.19.
Number: 1 .
Program 35 American earth weather satellite. 5 launches, 1962.05.24 (P 35-1) to 1963.09.27 (P 35-1). First US weather satellite, classified for many years. Predecessor to the DMSP series of military satellites. More...
Scout Solid-fuel, light payload, lower-cost launch vehicle developed by the Air Force and NASA in the late 1950's and used in a variety of configurations over thirty years. Launched from Cape Canaveral, Vandenberg, Wallops Island, and from Italy's equatorial San Marco platform off Kenya. Italy studied but did not develop subsequent upgraded versions. More...
Associated Manufacturers and Agencies
Vought American manufacturer of rockets and spacecraft. Vought, USA. More...
DMSP The first CORONA photos in August 1960 convinced authorities that knowledge of cloud cover over Russia was necessary and could be obtained only via satellite. Since the civilian TIROS program could not yet meet the requirement, the Director, National Reconnaissance Office authorized an 'interim' effort - the Defense Meteorological Satellite Program. The satellite series continued to be updated and served into the 21st Century. 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...
Vandenberg SLC5 Scout launch complex. Dedicated Scout launch pad, used during the life of that vehicle from 1962 to 1994. More...
Algol 2 Solid propellant rocket stage. Loaded/empty mass 11,600/1,650 kg. Thrust 564.25 kN. Vacuum specific impulse 255 seconds. More...
Antares 2 Solid propellant rocket stage. Loaded/empty mass 1,400/300 kg. Thrust 93.09 kN. Vacuum specific impulse 293 seconds. More...
Castor 1 Solid propellant rocket stage. Loaded/empty mass 3,852/535 kg. Thrust 286.00 kN. Vacuum specific impulse 247 seconds. More...
Scout X-3M Chronology
1963 February 19 -
16:33 GMT - .
. Launch Complex
: Vandenberg SLC5
. LV Family
. Launch Vehicle
: Scout X-3M
. LV Configuration
: Scout X-3M S126.
- P 35-3 - .
Mass: 40 kg (88 lb). Nation: USA. Agency: USAF. Program: DMSP. Class: Earth. Type: Weather satellite. Spacecraft: Program 35. Decay Date: 1979-12-26 . USAF Sat Cat: 533 . COSPAR: 1963-005A. Apogee: 810 km (500 mi). Perigee: 488 km (303 mi). Inclination: 100.5000 deg. Period: 97.80 min. Summary: Military weather satellite to provide targetting information for reconnaisance satellites..
Home - Browse - Contact
© / Conditions for Use