FIELD: rocketry and space engineering; pneumohydraulic and electric lines of multi-stage launch vehicle and their connection with ground lines. SUBSTANCE: oxidizer filling and vent pipe lines 13 and fuel filling and drain pipe lines 18, as well as plug connectors 24 for communication of launch vehicle with ground complex are mounted in separable module 2 located in parallel with axis of launch vehicle case 1; Module 2 is connected with case of launch vehicle by means of load-bearing detachable units provided with pushers. Case of module is divided by partition into two hermetic chambers: oxidizer chamber 10 and fuel chamber 11. Electric lines 22 and rocket drift engines are mounted on the outside of case of module 2. EFFECT: enhanced reliability. 3 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF FILLING MULTISTAGE LAUNCH VEHICLE | 1994 |
|
RU2081797C1 |
| UNIVERSAL HYDROGEN-OXYGEN ROCKET MODULE | 2015 |
|
RU2585210C1 |
| METHOD OF FILLING SPACE ROCKET SYSTEM OXIDISER TANKS WITH LIQUID OXYGEN | 2010 |
|
RU2455206C1 |
| LAUNCH VEHICLE | 1996 |
|
RU2101218C1 |
| METHOD FOR DELIVERY OF RAW MATERIAL TO ORBIT, ROCKET POWER PLANT, ROCKET ON ITS BASE, METHOD FOR INJECTION OF SPACE VEHICLES INTO GEOSTATIONARY ORBIT, TRANSPORTATION SYSTEM FOR ITS REALIZATION AND TRANSPORTATION-FUELING SYSTEM | 2003 |
|
RU2299160C2 |
| METHOD FOR PRE-LAUNCH PREPARATION OF LAUNCH VEHICLE WITH LIQUID-PROPELLANT ROCKET ENGINE USING GEL-LIKE ROCKET FUEL WITH POWDERED METAL ADDITIVE | 2023 |
|
RU2812496C2 |
| LAUNCH VEHICLE | 1995 |
|
RU2090465C1 |
| METHOD OF ROCKET TAKE-OFF | 2000 |
|
RU2170194C1 |
| METHOD FOR CLEANING OF ROCKET SEPARATING PART FROM LIQUID TOXIC REMAINS OF ROCKET FUEL COMPONENTS AND DEVICE FOR ITS REALISATION | 2007 |
|
RU2359876C1 |
| ROCKET LAUNCH COMPLEX WITH A ROCKET-CATAPULT VEHICLE FOR FLIGHTS TO THE MOON AND BACK | 2020 |
|
RU2743061C1 |
