发明名称 TOROIDAL TANK
摘要 rocketry; propellant system of launch vehicles. SUBSTANCE: tank includes upper and lower hermetic propellant reservoirs which are equipped with locking unit for coupling the cryogenic stage with launch vehicle (from below). Reservoirs have common intermediate bottom and single inner and outer shells. Upper reservoir which is coupled with payload at the top is provided with inner load-bearing taper envelope which is mounted inside reservoir and is secured to upper frame of this reservoir. Lower edge of envelope is secured to outer frame of intermediate bottom. Upper joint is coupled to inner shell of upper reservoir and lower joint is coupled to outer shell of lower reservoir. EFFECT: reduced mass of tanks; wide range of equipment used for making tank compartments. 1 dwg
申请公布号 RU2156722(C1) 申请公布日期 2000.09.27
申请号 RU19990124254 申请日期 1999.11.18
申请人 GOSUDARSTVENNYJ KOSMICHESKIJ NAUCHNO-PROIZVODSTVEN;G KOSM N PROIZV 发明人 KULAGA E.S.;VOSTRIKOV I.M.;PETROKOVSKIJ S.A.;SEVAL'NEV A.V.
分类号 B64G1/22;B64D37/00;B64G1/40;(IPC1-7):B64G1/22 主分类号 B64G1/22
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