FIELD: space engineering. SUBSTANCE: units for securing the external devices module and equipment compartment are interconnected by means of load-bearing members parallel to spacecraft axis and located tangentially relative to envelope of hermetic spacecraft casing. Point of attachment of external devices module and equipment compartment are turned over generatrix of envelope (body of revolution) towards each other relative to attachment units of equipment frame to envelope. Frame is made in form of hermetic compartment with walls parallel to longitudinal axis of spacecraft. Walls are provided with calibrated orifices for blowing the devices; seal is laid between walls and instruments. EFFECT: enhanced reliability. 2 cl, 2 dwg
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CASE OF SPACE VEHICLE INSTRUMENT MODULE | 1991 |
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Authors
Dates
1998-08-20—Published
1991-07-01—Filed