American all-solid orbital launch vehicle. Four stage vehicle consisting of 1 x Algol 3A + 1 x Castor 2 + 1 x Antares 2 + 1 x FW4S
LEO Payload: 183 kg (403 lb).
Gross mass: 20,600 kg (45,400 lb).
More... - Chronology...
Payload: 183 kg (403 lb).
Height: 25.00 m (82.00 ft).
Diameter: 1.14 m (3.74 ft).
Thrust: 464.00 kN (104,311 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 3A Solid propellant rocket stage. Loaded/empty mass 14,732/2,030 kg. Thrust 464.71 kN. Vacuum specific impulse 259 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...
Home - Browse - Contact
© / Conditions for Use