Heaob

Weight

154 kg

779 kg

Design Approach Primary structure Solar array

Equipment compartment Déployables

Central cylinder

Aluminum honeycomb panels deployed in two wings

Honeycomb panels mounted to longeron-stringer frame

Wrapped around or folded over equip compartment during boost

Semi-monocoque

Aluminum honeycomb panels body mounted

Honeycomb panels mounted to structural frame

TABLE 10-43. Estimated vs. Actual Sbes of FLTSATCOM and HEAO-B.

Spacecraft Parameters

Units

0 0

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