发明名称 UPPER-STAGE ROCKET
摘要 FIELD: transport. ^ SUBSTANCE: upper-stage rocket contains sustainer rocket engine, inter-tank girder, girder-link with carrier vehicle, and fuel tanks one of which has toroidal form and is inclined to longitudinal axis of upper-stage rocket. Toroidal form fuel tank has toroidal bottom gradually adjoint by outer spherical insert levelling it with external frame. Outer frame surface is perpendicular to longitudinal axis of upper-stage rocket and centre of outer spherical insert is located along longitudinal axis of upper-stage rocket. ^ EFFECT: increase of payload weight at expense of decrease of residual fuel in fuel tank, improvement of manufacturability and assembly of power modules. ^ 1 dwg
申请公布号 RU2341420(C2) 申请公布日期 2008.12.20
申请号 RU20060131228 申请日期 2006.08.30
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "RAKETNO-KOSMICHESKAJA KORPORATSIJA "EHNERGIJA" IMENI S.P. KOROLEVA" 发明人 KLIPPA VLADIMIR PETROVICH;PETRENKO STANISLAV ALEKSANDROVICH;SHTAN'KO EVGENIJ DMITRIEVICH;VESELOV VIKTOR NIKOLAEVICH;LAKEEEV VASILIJ NIKOLAEVICH;MERTVISHCHEV GRIGORIJ NIKOLAEVICH;GNEVSHEV VLADIMIR ALEKSANDROVICH;VOJTENKO KONSTANTIN ANATOL'EVICH;PROSELKOV ALEKSEJ VLADIMIROVICH;ROZHKOV MIKHAIL VIKTOROVICH
分类号 B64G1/40 主分类号 B64G1/40
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