Sustainer propulsion system

Power plants – Reaction motor – Plural motive fluid generating means or plural outlets

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Details

602701, 60 39142, 244 53B, 244 54, 244 55, 244135B, F02K 310

Patent

active

049380214

ABSTRACT:
The high cost of fabrication of a turbojet propulsion system 12 for a missile having an engine 18, mounted within a casing 14, including an inlet 20 to a compressor 22 and an exhaust gas outlet 24 is avoided in a structure having a propulsion system 12 with an inlet 26, 28; 37 located forward of the engine 18 for directing free stream air to the inlet 20 of the compressor 22, an outlet 30, 33; 38, 40 located aft of the engine 18 for directing exhaust gas into the free stream air, an engine starter 42 aft of the engine outlet 24, and a fuel storing bladder 46 forward of the engine 18.

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