The items identified as required to support the AMPS mission and requiring SR and T support and further work are: (1) a general purpose Experiment Pointing Mount; (2) a technique for measuring the attitude of the pallet-mounted or deployed experiments; (3) the development of a common optics cryogenically cooled interferometer spectrometer; (4) the development of a differential absorption lidar system for the measurement of ozone densitites in the earth's atmosphere; (5) the development of dc to dc power processors which are capable of converting energy stored in a capacitor system at 500 V to energy supplied to equipment operating at 40 kV and at 20 kW (eventually up to 100 kW); and (6) the development of a magnetic or possibly electrostati...
The science objectives, the experiment and instrument requirements, and the total ground and mission...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The economic and technical feasibility is assessed of employing a pallet-only mode for conducting At...
Engineering and operational facets associated with the implementation of the first two AMPS flights ...
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...
The physical, thermal, and electrical interfaces that exist between Spacelab-AMPS Payload No.(TBD) a...
The performance, design, verification and operational requirements for Labcraft equipment and Labcra...
The interfaces between AMPS Payload No.(TBD) and Spacelab are described. The interfaces specified co...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
Some 60 instrument candidates and 80 possible science investigations were evaluated. The early analy...
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....
An equipment list, instrument baseline data, engineering drawings, mass properties computer printout...
A data simulation is presented for instruments and associated control and display functions required...
The science objectives, the experiment and instrument requirements, and the total ground and mission...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The economic and technical feasibility is assessed of employing a pallet-only mode for conducting At...
Engineering and operational facets associated with the implementation of the first two AMPS flights ...
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...
The physical, thermal, and electrical interfaces that exist between Spacelab-AMPS Payload No.(TBD) a...
The performance, design, verification and operational requirements for Labcraft equipment and Labcra...
The interfaces between AMPS Payload No.(TBD) and Spacelab are described. The interfaces specified co...
Guidelines and general requirements applicable to the development of instrument flight hardware inte...
Some 60 instrument candidates and 80 possible science investigations were evaluated. The early analy...
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....
An equipment list, instrument baseline data, engineering drawings, mass properties computer printout...
A data simulation is presented for instruments and associated control and display functions required...
The science objectives, the experiment and instrument requirements, and the total ground and mission...
A study was conducted to derive and collect payload information on the anticipated space processing ...
The economic and technical feasibility is assessed of employing a pallet-only mode for conducting At...