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X90ALT-60000

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X90ALT-60000
Aerojet Nitric acid/Amine rocket engine. Development begun April 1947. Unspecified Application, 20,000 lbf subscale tested, new vertical test facility
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AKA: XLR23-AJ-1. First Launch: April 1947. Thrust: 264.00 kN (59,349 lbf).

Thrust (sl): 264.000 kN (59,349 lbf). Thrust (sl): 27,000 kgf. Propellant Formulation: Nitric acid/Aniline+Furfural Alcohol.

Family: Storable liquid. Country: USA. Propellants: Nitric acid/Amine. Agency: Aerojet.

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