Accession Number : AD0504273

Title :   Development and Qualification of the 40NS 4500 XM-24 Rocket Engine.

Descriptive Note : Technical note,

Corporate Author : WRIGHT AIR DEVELOPMENT CENTER WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Mallick,John

Report Date : NOV 1956

Pagination or Media Count : 10

Abstract : The development and the qualification test of the 40NS 4500 XM-24 solid rocket engine have been completed. The 40NS 4500 has passed the qualification test with some deviation to the low temperature requirements. The rocket engine is ready for flight testing on any aircraft which may require ATO. (Author)

Descriptors :   (*SOLID PROPELLANT ROCKET ENGINES, DESIGN), JATOS (U) BOOSTER ROCKETS, JET BOMBERS, TAKEOFF, PERFORMANCE(ENGINEERING), LOW TEMPERATURE, THRUST AUGMENTATION, OXIDIZERS, AMMONIUM COMPOUNDS, NITRATES, VIBRATION, CAPTIVE TESTS

Subject Categories : Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE