Add to ORKGThe baseline products, schedules, and resource requirements for the Mission Planning and Analysis Division's support of Space Transportation System flights 2, 3, and 4 are presented. Major functions addressed are: orbiter software, Mission Control Center software, flight design, flight operations support, simulation tools, and postflight analysis
A data link system used on a prototype autonomous roving vehicle is described. This system provides ...
The results of an effort to plan a final verification wind tunnel test to validate the recommended c...
An 0.8 percent fuel savings was achieved by a reduction in engine bleed air through the use of cabin...
General criteria for design of equipment and facilities to be used at Kennedy Space Cente
This document contains the design of the proportional estimate processor which was written to satisf...
The software utilized for image correction accuracy measurement is described. The correlation analys...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
The cost and programmatic considerations which integrate mission requirements and architectural opti...
A research and development program was successfully completed towards the development of a method of...
The level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
The performance of Bosch hardware at the subsystem level (up to five-person capacity) in terms of fi...
Utilization in the development of multi-kW low orbit power systems is discussed. The following techn...
The AEROX aerodynamic computer program which provides accurate predictions of induced drag and trim ...
The computer code for the trajectory processor (#TRAJ) of the high fidelity relative motion program ...
An algorithm for using electric currents to control pendular oscillations induced by various perturb...
A data link system used on a prototype autonomous roving vehicle is described. This system provides ...
The results of an effort to plan a final verification wind tunnel test to validate the recommended c...
An 0.8 percent fuel savings was achieved by a reduction in engine bleed air through the use of cabin...
General criteria for design of equipment and facilities to be used at Kennedy Space Cente
This document contains the design of the proportional estimate processor which was written to satisf...
The software utilized for image correction accuracy measurement is described. The correlation analys...
A three-person capacity preprototype vapor compression distillation subsystem for recovering potable...
The cost and programmatic considerations which integrate mission requirements and architectural opti...
A research and development program was successfully completed towards the development of a method of...
The level C requirements for the shuttle orbiter terminal area energy management (TAEM) guidance and...
The performance of Bosch hardware at the subsystem level (up to five-person capacity) in terms of fi...
Utilization in the development of multi-kW low orbit power systems is discussed. The following techn...
The AEROX aerodynamic computer program which provides accurate predictions of induced drag and trim ...
The computer code for the trajectory processor (#TRAJ) of the high fidelity relative motion program ...
An algorithm for using electric currents to control pendular oscillations induced by various perturb...
A data link system used on a prototype autonomous roving vehicle is described. This system provides ...
The results of an effort to plan a final verification wind tunnel test to validate the recommended c...
An 0.8 percent fuel savings was achieved by a reduction in engine bleed air through the use of cabin...