The development of space shuttle separation devices is reviewed to illustrate the mechanisms involved in separating the Orbiter from the Boeing 747 carrier aircraft and from the externally mounted propellant tank. Other aspects of the separation device development discussed include design evolution, operational experience during the orbiter approach and landing tests, and the work required to produce an operational system
Iterative procedures were used to analyze the performance of two preliminary shuttle/GPS navigation ...
The Level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
The definition of standard flight segments of phases, representing flight profile components which c...
A preflight analysis of the ALT separation reference trajectories for the tailcone on, forward, and ...
Space shuttle guidance, navigation, and control design equations are presented. The space-shuttle mi...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
A series of microwave measurements was conducted to determine the radar cross section of the Space S...
A preliminary spacecraft servicing demonstration plan is prepared which leads to a fully verified op...
A guidance, navigation, and control system, the Simulated Shuttle Flight Test System (SS-FTS), when ...
The STS-51 Space Shuttle Program Mission Report summarizes the payloads as well as the orbiter, exte...
An orbiter/IUS separation sequence to satisfy the assumed requirements of Shuttle Flight 8 was defin...
Multidisciplined advanced planning studies were conducted that involve space operations and the asso...
This Space Transportation System 7 (STS-7) Flight Feasibility Assessment (FFA) provides a base from ...
The proximity translation and final docking of the space teleoperator evaluation vehicle (STEV) with...
Iterative procedures were used to analyze the performance of two preliminary shuttle/GPS navigation ...
The Level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
The definition of standard flight segments of phases, representing flight profile components which c...
A preflight analysis of the ALT separation reference trajectories for the tailcone on, forward, and ...
Space shuttle guidance, navigation, and control design equations are presented. The space-shuttle mi...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
A series of microwave measurements was conducted to determine the radar cross section of the Space S...
A preliminary spacecraft servicing demonstration plan is prepared which leads to a fully verified op...
A guidance, navigation, and control system, the Simulated Shuttle Flight Test System (SS-FTS), when ...
The STS-51 Space Shuttle Program Mission Report summarizes the payloads as well as the orbiter, exte...
An orbiter/IUS separation sequence to satisfy the assumed requirements of Shuttle Flight 8 was defin...
Multidisciplined advanced planning studies were conducted that involve space operations and the asso...
This Space Transportation System 7 (STS-7) Flight Feasibility Assessment (FFA) provides a base from ...
The proximity translation and final docking of the space teleoperator evaluation vehicle (STEV) with...
Iterative procedures were used to analyze the performance of two preliminary shuttle/GPS navigation ...
The Level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi