A method is described for placing a large, STS-compatible platform on orbit utilizing a construction method employing both deployable and erectable structures. A multifunctional mechanism is used for deployable structures and an on-orbit assembly is used for erectable structures. Also analyses are discussed which assess the thermal distortion of a simple open truss and a more complex truss.
Structural/thermal considerations for design of large space platform structures
1978-01-01
Conference paper
No indication
English
Some Design Considerations for Large Space Structures
AIAA | 1978
|Some design considerations for large space structures
AIAA | 1977
|Large space platform control avionics considerations
NTRS | 1978
|