AJ10-33 (original) (raw)

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AJ10-33

Aerojet Nitric acid/UDMH rocket engine. SMART Sled. Development begun early 1950s. 114,000 lbf thrust, uncooled, ceramic lined, 3 chamber system

Date: Early 1950s. Thrust: 509.00 kN (114,427 lbf).

Propellant Formulation: IRFNA/UDMH.

Subtopics

AJ10-51 Aerojet rocket engine. Sled. Thrust variable to 33% indicated.

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

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