Problems encountered in providing h-p hot-gas source to turbine of aircraft engine starter, methods of solving these problems, and design procedures followed in arriving at solid-propellant cartridge which functioned in all environments encountered in both storage and operation; development techniques and results of experimental investigations are presented.
Development of cartridges for aircraft engine cartridge starters
ASME -- Paper
ASME Meeting GT-21 ; 1967 Starting
1967
11 pages
Aufsatz (Konferenz)
Englisch
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