THRUST PULSE OUTPUT SYSTEM

FIELD: aircraft engineering.SUBSTANCE: proposed system comprises control system, spherical tanks with deforming metal webs separating fuel and gas chambers, balloons, filling necks, low-thrust liquid-propellant control engine units, correction-braking engine, chokes, air-operated electrical valves,...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	VASIL'EV VALERIJ ALEKSEEVICH, KAZAKOV VLADIMIR EVGEN'EVICH, MAKAR'JANTS MIKHAIL VIKTOROVICH, STRAMOUSOV VALERIJ ALEKSANDROVICH, BOLTOV ELISEJ ALEKSANDROVICH, POPOVA OL'GA PETROVNA, GOLEVA TAT'JANA VASIL'EVNA, AKSAMENTOV MIKHAIL JUR'EVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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