| 发明名称 |
MULTISTAGE LAUNCH VEHICLE |
| 摘要 |
FIELD: rocketry and space engineering; designing launch vehicles for injection of various payloads into near-earth orbit. SUBSTANCE: multistage launch vehicle has rocket pods of first and second stages connected by parallel pattern. Additional propellant tank connected to propellant compartment of rocket pod of second stage of launch vehicle through main fitted with cut-off valve which is separated in flight is located coaxially relative to first stage. Additional propellant tank is also connected with inter-pod adapter compartment. Rocket pods of first and second stage are connected by means of load-bearing connection units located on their lateral surfaces. EFFECT: increased relative mass of payload and improved operational parameters of multistage launch vehicle. 3 dwgv
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| 申请公布号 |
RU2116941(C1) |
申请公布日期 |
1998.08.10 |
| 申请号 |
RU19970100448 |
申请日期 |
1997.01.10 |
| 申请人 |
BELJANIN EHDUARD VALENTINOVICH;VELICHKO IGOR' IVANOVICH;GLADYSHEV SERGEJ VLADIMIROVICH;IVANOV MIKHAIL JUR'EVICH;KATORGIN BORIS IVANOVICH;MOGILENKO VLADIMIR IVANOVICH;OBUKHOV NIKOLAJ ALEKSANDROVICH;RACHUK VLADIMIR SERGEEVICH;SOKOLOV BORIS ALEKSANDROVICH;TUPITSYN NIKOLAJ NIKOLAEVICH;CHVANOV VLADIMIR KONSTANTINOVICH |
发明人 |
BELJANIN EH.V.;VELICHKO I.I.;GLADYSHEV S.V.;IVANOV M.JU.;KATORGIN B.I.;MOGILENKO V.I.;OBUKHOV N.A.;RACHUK V.S.;SOKOLOV B.A.;SYROVETS M.N.;TUPITSYN N.N.;CHVANOV V.K. |
| 分类号 |
B64G1/00;(IPC1-7):B64G1/00 |
主分类号 |
B64G1/00 |
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