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X60ALD-4000
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Manufacturer Name: X60ALD-4000. Government Designation: XLR13-AJ-1. Designer: Aerojet. Developed in: May 1946. Application: ATO for XB-45, B-45A. Propellants: Nitric acid/Amine. Thrust(sl): 17.600 kN (3,957 lbf). Burn time: 60 sec. Mass Engine: 363 kg (800 lb). Diameter: 0.81 m (2.65 ft). Length: 3.43 m (11.25 ft). Chamber Pressure: 21.00 bar. Country: USA. Development begun May 1946. Pressurising tank surrounded propellant tanks. Regeneratively cooled. Parachute for dropping and recovery after takeoff. Later redesigned to use WFNA and gasoline.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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