FIELD: rocket engineering. SUBSTANCE: combination ramjet-rocket engine has sustainer engine and combustion chamber of ramjet engine communicating with air intake. Launching engine is located in combustion chamber in two ring belts with units of radial fixing. One of ring belts is fitted with units of axial fixing. EFFECT: expanded range of application of engine, provision for shockless removal of launching engine from rests. 4 dwg
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Authors
Dates
1994-06-30—Published
1992-09-01—Filed