OAM

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OAM

Hydrazine propellant rocket stage. Monopropellant final stage providing precise orbital injection. Pressure-fed, indefinite number of restarts.

Status: Out of production. Thrust: 882 N (198 lbf). Gross mass: 714 kg (1,574 lb). Unfuelled mass: 360 kg (790 lb). Specific impulse: 222 s. Burn time: 1,500 s. Height: 1.00 m (3.20 ft). Diameter: 2.30 m (7.50 ft). Span: 2.30 m (7.50 ft).

No Engines: 4.

Country: USA. Engines: MR-107. Launch Vehicles: Athena-1, Athena-2, Athena-3, Satellite Launch Vehicle.

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