RM-100B

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RM-100B

Part of RM-100A

RM-100B
Credit: Boeing / Rocketdyne

Rocketdyne Nitric acid/UDMH rocket engine. Satellite Reaction Control. Pressure-fed.

Date: 1967. Thrust: 441 N (99 lbf). Specific impulse: 283 s.

Propellant Formulation: IRFNA/MDMH.

Family: Storable liquid. Country: USA. Propellants: Nitric acid/UDMH. Agency: Rocketdyne.

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