FIELD: rocket engineering. SUBSTANCE: invention refers to instrument containers which bodies are used as load-bearing members of structure. Part of load-bearing base 4 of sealed container with electron equipment and lower envelope 5 of same container are employed as load-bearing member of bracing unit and other parts have smaller mass in this case. This is achieved by strengthening of side surfaces of load-bearing base during installation of straight-through electric connector assemblies 11 in them and by fabrication of lower envelope 5 in the form of sloping spherical strengthening shell. Upper envelope 6 has toroidal-conical-spherical shape. EFFECT: improved mass and size characteristics of stage by perfecting load-bearing configuration of sealed container with electron equipment taking loads. 4 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| ROCKET INSTRUMENT SECTION | 1991 | 
 | RU2103654C1 | 
| SPACE SHIP | 1992 | 
 | RU2021172C1 | 
| MICRO-SATELLITE | 2004 | 
 | RU2268205C2 | 
| SMALL BOOSTER | 2023 | 
 | RU2808312C1 | 
| SPACE ROCKET SYSTEM AND METHOD FOR RENDERING SERVICES IN LAUNCHING SPACE VEHICLES USING SPACE ROCKET SYSTEM | 2001 | 
 | RU2179941C1 | 
| SPACECRAFT | 1991 | 
 | RU2117609C1 | 
| SET OF ACCESSORIES FOR VIBRATION TESTING OF ELECTRONIC EQUIPMENT AS PART OF CYLINDRICAL COMPARTMENT AND METHOD OF VIBRATION TESTING | 2024 | 
 | RU2840777C1 | 
| ROCKET STAGE | 2000 | 
 | RU2193994C2 | 
| DAMPENING UNIT FOR FUEL TANK | 2002 | 
 | RU2231669C2 | 
| SPACE HEAD MODULE FOR ISOLATED AND CLUSTER LAUNCH OF SATELLITES | 2005 | 
 | RU2293689C2 | 
Authors
Dates
1998-10-20—Published
1990-07-17—Filed