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RM-100B


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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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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