Scout A through G

Scout launch vehicle
Image by NASA

Country of Origin: United States
Manufacturer: NASA, Aerojet, Thiokol, Allegany Ballistics Lab

Height: 23 – 25 m
Diameter: 1.01 m
Payload to LEO: 173 kg
Total Mass: 17.85 – 21.5 tons

Launch Sites: Cape Canaveral, Wallops, Vandenberg
First Flight: April 18, 1960; (first orbit: February 16, 1961)
Last Flight: May 9, 1994
Total Launches: 71
Successful Launches: 68

 

 

Scout A

Stage Diameter Fuel Engine Time Thrust (Vac.) ISP (SL / Vac.) Mass / Empty Mass
1 (Algol) 1.01 m Solid Algol 47 s 564.25 kN 211 s / ? 11.6 tons / 1.65 tons
2 (Castor) 0.79 m Solid XM33 Castor 37 s 268.92 kN ? / 272.6 s 4.424 tons / 0.695 tons
3 (Antares) 0.78 m Solid X-254 Antares 36 s 93.09 kN ? / 282 s 1.4 tons / 0.3 tons
4 (Altair) 0.64 m Solid X-248 Altair 28 s 22.24 kN ? / 265.9 s 275 kg / 37 kg

 

 

Scout G

Stage Diameter Fuel Engine Time Thrust (Vac.) ISP (SL / Vac.) Mass / Empty Mass
1 (Algol) 1.14 m Solid UTC 56 s 621 kN 233 s / ?
2 (Castor) 0.79 m Solid TX-354-3 37 s 268.92 kN ? / 272.6 s
3 (Antares) 0.76 m Solid TE-M-762 45.4 s 82.3 kN ? / 296 s
4 (Altair) 0.50 m Solid TE-M-640-1 31.6 s 24.47 kN ? / 288.4 s

 

 

 

 

Links:

b14643.de

Wikipedia

Destination Orbite – Scout X

Destination Orbite – Scout A through G

Encyclopedia Astronautica

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