American all-solid orbital launch vehicle. Four stage vehicle consisting of 1 x Algol 2A + 1 x Castor 2 + 1 x Antares 2 + 1 x FW4S
LEO Payload: 143 kg (315 lb).
Gross mass: 17,000 kg (37,000 lb).
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Payload: 143 kg (315 lb).
Height: 22.00 m (72.00 ft).
Thrust: 400.00 kN (89,920 lbf).
Apogee: 1,000 km (600 mi).
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...
Algol 2 Solid propellant rocket stage. Loaded/empty mass 11,600/1,650 kg. Thrust 564.25 kN. Vacuum specific impulse 255 seconds. More...
Altair 3 Solid propellant rocket stage. Loaded/empty mass 301/25 kg. Thrust 27.40 kN. Vacuum specific impulse 280 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 2 Solid propellant rocket stage. Loaded/empty mass 4,424/695 kg. Thrust 258.92 kN. Vacuum specific impulse 262 seconds. More...
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