FIELD: rocketry. SUBSTANCE: invention relates to fastening of electrical equipment on launch vehicle. Proposed fastening unit consists of two parts secured on corresponding parts of electrical connector. One of said parts has beams made over generating surface of bottoms on toroidal tank. Beams thrust by one end against brackets installed on butt-joining envelopes of toroidal tank with other tanks of launch vehicle. Other ends of beams rest on brackets installed on tank frame. Split part in form of plate is mounted on beams. EFFECT: reduced mass of fastening unit, provision of compactness, reliability and convenience in operation for design versions of launch vehicles. 2 cl, 1 dwg _
| Title | Year | Author | Number |
|---|---|---|---|
| TOROIDAL TANK | 1999 |
|
RU2156722C1 |
| UNIT FOR CONNECTION OF STAGES OF CRYOGENIC STAGE | 1999 |
|
RU2179942C2 |
| LAUNCH VEHICLE COMPARTMENT | 2001 |
|
RU2209156C1 |
| ROCKET POD (VERSIONS) AND METHOD OF ITS MANUFACTURE (VERSIONS) | 2000 |
|
RU2191720C2 |
| ROCKET POD | 2002 |
|
RU2232699C1 |
| LAUNCH VEHICLE PROPELLANT TANK UNIT | 1999 |
|
RU2151718C1 |
| CRYOGENIC STAGE | 1999 |
|
RU2156723C1 |
| MULTI-PURPOSE SYSTEM FOR PREPARATION AND LAUNCH OF SPACE ROCKETS OF DIFFERENT CLASSES | 2000 |
|
RU2194654C2 |
| INSTRUMENT MODULE CASE | 1999 |
|
RU2159202C1 |
| CARRIER ROCKET | 2007 |
|
RU2331550C1 |
