AJ10-28

Engine · USA

Original archive entry. The text, images and links below are kept as they were written.

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.

Propellant Formulation: RFNA/JP-X.

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

Related