Delta 104 (original) (raw)

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Delta 104

Part of Delta

Nitric acid/UDMH propellant rocket stage. .

Status: Retired 1962. Thrust: 35.10 kN (7,890 lbf). Gross mass: 4,472 kg (9,859 lb). Unfuelled mass: 590 kg (1,300 lb). Specific impulse: 278 s. Burn time: 296 s. Height: 5.88 m (19.29 ft). Diameter: 1.40 m (4.50 ft). Span: 1.40 m (4.50 ft).

Cost $ : 1.740 million.

Country: USA. Engines: AJ10-104. Launch Vehicles: Thor Delta. Propellants: Nitric acid/UDMH.

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