A summary of findings of the Flight Elements Subpanel is given in viewgraph form. Topics covered include advanced avionics architecture; processors; integrated Global Positioning System and guidance, navigation and control; displays and controls; telemetry; sensors and instrumentation; fault detection and management; electrical power distribution and control; spacecraft power supplies; and in-flight crew training
An improvement is presented for the 2-D strategies for adjustment of the flexible top and bottom wal...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
The objective of this study is to apply the integrated design methodology to the mature GOES-1 space...
Space transportation avionics technology operational efficiency issues are presented in viewgraph fo...
Orbiter Orbital Maneuver Subsystem (OMS) and Reaction Control Subsystem (RCS) tankage has proved to ...
An outline of the organization and capabilities of the Engine Structures Computational Simulator (Si...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...
Vugraphs are presented on the effect of cruise Mach number on the maximum takeoff weight of the High...
The CORPUS (Computation Of Retarded Propagation Under Spectrum loading) crack growth prediction mode...
Some preliminary results of research on control of flexible structures performed at the Jet Propulsi...
The objective is to develop, access, and implement software management aids, leading to an environme...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Several tests of the Rocketdyne configuration of the Space Shuttle Main Engine (SSME) High Pressure ...
For substantiation of the recently certified medium range Airbus A330 and long range A340 the full s...
An improvement is presented for the 2-D strategies for adjustment of the flexible top and bottom wal...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
The objective of this study is to apply the integrated design methodology to the mature GOES-1 space...
Space transportation avionics technology operational efficiency issues are presented in viewgraph fo...
Orbiter Orbital Maneuver Subsystem (OMS) and Reaction Control Subsystem (RCS) tankage has proved to ...
An outline of the organization and capabilities of the Engine Structures Computational Simulator (Si...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...
Vugraphs are presented on the effect of cruise Mach number on the maximum takeoff weight of the High...
The CORPUS (Computation Of Retarded Propagation Under Spectrum loading) crack growth prediction mode...
Some preliminary results of research on control of flexible structures performed at the Jet Propulsi...
The objective is to develop, access, and implement software management aids, leading to an environme...
The Space Station structure has been baselined to be a 5 M (16.4 ft) erectable truss. This structure...
Several tests of the Rocketdyne configuration of the Space Shuttle Main Engine (SSME) High Pressure ...
For substantiation of the recently certified medium range Airbus A330 and long range A340 the full s...
An improvement is presented for the 2-D strategies for adjustment of the flexible top and bottom wal...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
The objective of this study is to apply the integrated design methodology to the mature GOES-1 space...