FIELD: rocketry; cryogenic stages of launch vehicles at coaxial arrangement of stages. SUBSTANCE: instrument module case includes instrument frame and load-bearing taper envelope with end frames. Frame of lower portion of envelope is provided with web for coupling with propellant tank of second stage. Upper frame of envelope has web in its lower portion for coupling with instrument frame and web in center portion for coupling with first and second stages of cryogenic stage. Locks fitted in upper portion of frame are used for coupling the payload with cryogenic stage. EFFECT: reduction of mass of instrument module case. 1 dwg
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| TOROIDAL TANK | 1999 |
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| METHOD FOR ORBIT INJECTION OF PAYLOAD BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINATION ARRANGEMENT WITH CRUISE LIQUID- PROPELLANT ROCKET ENGINE INSTALLATIONS (LREI), MULTIFUNCTIONAL LAUNCH VEHICLE WITH CRUISE LPEI AND METHOD FOR ITS DEVELOPMENT | 2000 |
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RU2161108C1 |
