Add to ORKGThe physical, thermal, and electrical interfaces that exist between Spacelab-AMPS Payload No.(TBD) and the orbiter are described
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...
General physical, functional, and operational interface control requirements for instruments on the ...
A detailed analysis is presented of each selected equipment item, and suitability and cost analyses ...
The interfaces between AMPS Payload No.(TBD) and Spacelab are described. The interfaces specified co...
The electrical, mechanical, and environmental interfaces between the boom-mounted flux gate magnetom...
The interfaces between the scientific instruments and the Spacelab/Labcraft equipment are described....
Engineering and operational facets associated with the implementation of the first two AMPS flights ...
The performance, design, verification and operational requirements for Labcraft equipment and Labcra...
The items identified as required to support the AMPS mission and requiring SR and T support and furt...
The AMPS Flight 2 payload, its operation, and the support required from the Space Transportation Sys...
The results are presented of the AMPS Phase C/D (Design, Development, and Operations) program analys...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
An equipment list, instrument baseline data, engineering drawings, mass properties computer printout...
Some 60 instrument candidates and 80 possible science investigations were evaluated. The early analy...
The quantification of required specimen(s) from space processing experiments, the typical EMI measur...
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...
General physical, functional, and operational interface control requirements for instruments on the ...
A detailed analysis is presented of each selected equipment item, and suitability and cost analyses ...
The interfaces between AMPS Payload No.(TBD) and Spacelab are described. The interfaces specified co...
The electrical, mechanical, and environmental interfaces between the boom-mounted flux gate magnetom...
The interfaces between the scientific instruments and the Spacelab/Labcraft equipment are described....
Engineering and operational facets associated with the implementation of the first two AMPS flights ...
The performance, design, verification and operational requirements for Labcraft equipment and Labcra...
The items identified as required to support the AMPS mission and requiring SR and T support and furt...
The AMPS Flight 2 payload, its operation, and the support required from the Space Transportation Sys...
The results are presented of the AMPS Phase C/D (Design, Development, and Operations) program analys...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
An equipment list, instrument baseline data, engineering drawings, mass properties computer printout...
Some 60 instrument candidates and 80 possible science investigations were evaluated. The early analy...
The quantification of required specimen(s) from space processing experiments, the typical EMI measur...
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...
General physical, functional, and operational interface control requirements for instruments on the ...
A detailed analysis is presented of each selected equipment item, and suitability and cost analyses ...