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Scout D
Part of Scout Family
Scout D1
Scout D1
Scout D1 - COSPAR 1979-047
American all-solid orbital launch vehicle.

Status: Out of production. Payload: 185 kg (407 lb). Thrust: 395.50 kN (88,912 lbf). Gross mass: 20,670 kg (45,560 lb). Height: 25.00 m (82.00 ft). Diameter: 1.14 m (3.74 ft). Apogee: 185 km (114 mi).

LEO Payload: 185 kg (407 lb) to a 185 km orbit. Flyaway Unit Cost 1985$: 8.660 million.

Stage Data - Scout D

  • Stage 1. 1 x Algol 3. Gross Mass: 14,320 kg (31,570 lb). Empty Mass: 1,600 kg (3,500 lb). Thrust (vac): 471.905 kN (106,088 lbf). Isp: 284 sec. Burn time: 75 sec. Isp(sl): 238 sec. Diameter: 1.14 m (3.74 ft). Span: 1.14 m (3.74 ft). Length: 9.40 m (30.80 ft). Propellants: Solid. No Engines: 1. Engine: Algol 3. Status: In Production.
  • Stage 2. 1 x Castor 2. Gross Mass: 4,424 kg (9,753 lb). Empty Mass: 695 kg (1,532 lb). Thrust (vac): 258.915 kN (58,206 lbf). Isp: 262 sec. Burn time: 37 sec. Isp(sl): 232 sec. Diameter: 0.79 m (2.59 ft). Span: 0.79 m (2.59 ft). Length: 6.04 m (19.81 ft). Propellants: Solid. No Engines: 1. Engine: TX-354-3. Status: In Production.
  • Stage 3. 1 x Antares 2. Gross Mass: 1,400 kg (3,000 lb). Empty Mass: 300 kg (660 lb). Thrust (vac): 93.094 kN (20,928 lbf). Isp: 293 sec. Burn time: 36 sec. Isp(sl): 233 sec. Diameter: 0.78 m (2.55 ft). Span: 0.78 m (2.55 ft). Length: 2.90 m (9.50 ft). Propellants: Solid. No Engines: 1. Engine: X-259. Status: Out of Production.
  • Stage 4. 1 x Altair 3. Gross Mass: 301 kg (663 lb). Empty Mass: 25 kg (55 lb). Thrust (vac): 27.400 kN (6,160 lbf). Isp: 280 sec. Burn time: 27 sec. Isp(sl): 255 sec. Diameter: 0.64 m (2.09 ft). Span: 0.64 m (2.09 ft). Length: 2.53 m (8.30 ft). Propellants: Solid. No Engines: 1. Engine: FW-4S, TEM640. Status: Out of Production.

Family: all-solid, orbital launch vehicle. Country: USA. Spacecraft: Transit, Ariel, San Marco satellite, ESRO, SAS, MTS, TIP, AEROS, Miranda, Hawkeye, ANS, AEM, SAGE, HILAT. Stages: Algol 3, Antares 2, Altair 3, Castor 2. Agency: Vought.


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