Add to ORKGThe results are presented of the AMPS Phase C/D (Design, Development, and Operations) program analysis and planning effort. Cost and schedule estimates are included. Although the AMPS program has been specifically addressed, these task descriptions are basically adaptable to a broader-based program incorporating additional or different Spacelab/orbiter payloads
The AMPS Program Specification delineates the AMPS Program requirements consistent with the resource...
The services provided by the Spacelab Information Management System are discussed. The majority of t...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
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...
Some 60 instrument candidates and 80 possible science investigations were evaluated. The early analy...
The AMPS Flight 2 payload, its operation, and the support required from the Space Transportation Sys...
The items identified as required to support the AMPS mission and requiring SR and T support and furt...
The interfaces between the scientific instruments and the Spacelab/Labcraft equipment are described....
The interfaces between AMPS Payload No.(TBD) and Spacelab are described. The interfaces specified co...
The physical, thermal, and electrical interfaces that exist between Spacelab-AMPS Payload No.(TBD) a...
An equipment list, instrument baseline data, engineering drawings, mass properties computer printout...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
The electrical, mechanical, and environmental interfaces between the boom-mounted flux gate magnetom...
Typical missions identified for AMPS flights in the arly 1980's are described. Experiment objectives...
The AMPS Program Specification delineates the AMPS Program requirements consistent with the resource...
The services provided by the Spacelab Information Management System are discussed. The majority of t...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
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...
Some 60 instrument candidates and 80 possible science investigations were evaluated. The early analy...
The AMPS Flight 2 payload, its operation, and the support required from the Space Transportation Sys...
The items identified as required to support the AMPS mission and requiring SR and T support and furt...
The interfaces between the scientific instruments and the Spacelab/Labcraft equipment are described....
The interfaces between AMPS Payload No.(TBD) and Spacelab are described. The interfaces specified co...
The physical, thermal, and electrical interfaces that exist between Spacelab-AMPS Payload No.(TBD) a...
An equipment list, instrument baseline data, engineering drawings, mass properties computer printout...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
The electrical, mechanical, and environmental interfaces between the boom-mounted flux gate magnetom...
Typical missions identified for AMPS flights in the arly 1980's are described. Experiment objectives...
The AMPS Program Specification delineates the AMPS Program requirements consistent with the resource...
The services provided by the Spacelab Information Management System are discussed. The majority of t...
Examination of commercial equipment technologies revealed that the functional performance requiremen...