The patent relates to a solid fuel ramjet powered missile having the air inlets positioned adjacent the aft end of the fuel grain with a channel provided adjacent the fuel grain to provide primary air into the forward end of the fuel grain. The secondary air is supplied directly to the secondary combustor. A valve is provided in the primary air flow channel to control the air flow into the fuel grain.
AFT Inlet Ramjet Powered Missile
1973
3 pages
Report
Keine Angabe
Englisch
Aft Inlet Ramjet Powered Missile
NTIS | 1973
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