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AJ10-28
Aerojet Nitric acid/JP-X rocket engine. SNORT Sled. Development begun early 1950s. 35,000 lbf thrust, 2-10 second duration. JP-X was a jet fuel / hydrazine mixture.

Date: Early 1950s. Thrust: 156.00 kN (35,070 lbf).

Propellant Formulation: RFNA/JP-X.

Family: Storable liquid. Country: USA. Propellants: Nitric acid/JP-X. Agency: Aerojet.
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