GYRATING ROCKET STAGE WITH COMBINED POWER PLANT AND METHOD OF CONTROLLING ROCKET FLIGHT

FIELD: transport. ^ SUBSTANCE: invention relates to rocketry. Gyrating stage comprises nose section and gas generator with pushing, pulling and bank control nozzles. Additionally, said stage comprises sustainer communicated via gas dust and bypass valve with gas generator. Sustainer incorporates thr...

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Bibliographische Detailangaben
Hauptverfasser: LOSHKAREV ANATOLIJ NIKOLAEVICH, ALIEV ALI VEJSOVICH, SERMJAGIN KONSTANTIN VIKTOROVICH, MIRONOV ANDREJ NIKOLAEVICH
Format: Patent
Sprache:eng ; rus
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