The AMPS to Spacelab Interface Control Document which is to be used as a guide for format and information content in generating specific AMPS Mission ICDs is presented. This document is meant to supplement the Spacelab Payload Accommodations Handbook in that it only defines interfaces which are not discussed in the handbook to the level required for design purposes. The AMPS Top Level Requirements Tree, illustrates this ICD by a shaded area and its relationship to the other AMPS technical documents. Other interface documents shown are the Level II, AMPS to Space Shuttle Vehicle ICD and the Level III, AMPS to Instruments ICD
Tracking and data acquisition system (TDAS) requirements, TDAS architectural goals, enhanced TDAS su...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
Low thrust chemical (hydrogen-oxygen) propulsion systems configured specifically for low acceleratio...
Physical, functional, and operational interfaces between the space shuttle orbiter and the AMPS payl...
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
A set of hardware similar to the SEASAT A configuration requirement, suitable for installation and o...
Guidelines are presented for instrument/experiment developers concerning hardware design, flight ver...
The development of large space structure (LSS) technology is discussed, with emphasis on space fabri...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
A preliminary feasibility study of the microwave multi-applications payload (MMAP) system for the Sp...
Engineering and performance of warm gas mass expulsion system for attitude control on long space voy...
Mathematical models and orbital mechanics for space shuttle guidance, control, and navigation during...
An energetic experiment using the Z80 family of microcomputer components is described. Data collecte...
The Jupiter Orbiter as it is presently understood is documented. Because the Jupiter Orbiter Probe 1...
Data sheets are presented for 11 internal payloads, 30 externally mounted payloads, and 46 free flye...
Tracking and data acquisition system (TDAS) requirements, TDAS architectural goals, enhanced TDAS su...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
Low thrust chemical (hydrogen-oxygen) propulsion systems configured specifically for low acceleratio...
Physical, functional, and operational interfaces between the space shuttle orbiter and the AMPS payl...
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
A set of hardware similar to the SEASAT A configuration requirement, suitable for installation and o...
Guidelines are presented for instrument/experiment developers concerning hardware design, flight ver...
The development of large space structure (LSS) technology is discussed, with emphasis on space fabri...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
A preliminary feasibility study of the microwave multi-applications payload (MMAP) system for the Sp...
Engineering and performance of warm gas mass expulsion system for attitude control on long space voy...
Mathematical models and orbital mechanics for space shuttle guidance, control, and navigation during...
An energetic experiment using the Z80 family of microcomputer components is described. Data collecte...
The Jupiter Orbiter as it is presently understood is documented. Because the Jupiter Orbiter Probe 1...
Data sheets are presented for 11 internal payloads, 30 externally mounted payloads, and 46 free flye...
Tracking and data acquisition system (TDAS) requirements, TDAS architectural goals, enhanced TDAS su...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
Low thrust chemical (hydrogen-oxygen) propulsion systems configured specifically for low acceleratio...