Requirements are presented for the ascent/descent (A/D) navigation and attitude-dependent ancillary data products to be generated for the space shuttle orbiter in support of orbital flight test requirements, MPAD guidance and navigation performance assessment, and the mission evaluation team. It was intended that this document serve as the sole requirements control instrument between MPB/MPAD and the A/D ancillary data users. The requirements are primarily functional in nature, but some detail level requirements are also included
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
Candidate vertical control systems (VCS) and face advancement systems (FAS) required to satisfactori...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
Requirements are presented for the ascent/descent (A/D) navigation and attitude-dependent ancillary ...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
Physical, functional, and operational interfaces between the space shuttle orbiter and the AMPS payl...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
Checkout and data management system requirements for space station and space base mission progra
The performance of satellite subsystems and the response of in-orbit payload systems are summarized....
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...
The formulation and implementation of navigation systems used for research investigations in the V/S...
A consumables analysis of the environmental control and life support system (ECLSS) was performed fo...
Service equipment mission requirements are discussed. On-orbit operations, satellite classes, and re...
Guidelines are presented for instrument/experiment developers concerning hardware design, flight ver...
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
Candidate vertical control systems (VCS) and face advancement systems (FAS) required to satisfactori...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
Requirements are presented for the ascent/descent (A/D) navigation and attitude-dependent ancillary ...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
Physical, functional, and operational interfaces between the space shuttle orbiter and the AMPS payl...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
Checkout and data management system requirements for space station and space base mission progra
The performance of satellite subsystems and the response of in-orbit payload systems are summarized....
Advanced studies are reviewed. Atmospheric sciences, magnetospheric physics, solar physics, gravitat...
The formulation and implementation of navigation systems used for research investigations in the V/S...
A consumables analysis of the environmental control and life support system (ECLSS) was performed fo...
Service equipment mission requirements are discussed. On-orbit operations, satellite classes, and re...
Guidelines are presented for instrument/experiment developers concerning hardware design, flight ver...
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
Candidate vertical control systems (VCS) and face advancement systems (FAS) required to satisfactori...