The performance of the Kuband radar was analyzed in detail, and the performance was updated and summarized. In so doing, two different radar design philosophies were described, and the corresponding differences in losses were enumerated. The resulting design margins were determined for both design philosophies and for both the designated and nondesignated range modes of operation. In some cases, the design margin was about zero, and in other cases it was significantly less than zero. With the point of view described above, the recommended solution is to allow more scan time but at the present scan rate. With no other changes in the present configuration, the radar met design detection specifications for all design philosophies at a range of...
The L-band positioning experiment is reported which encompassed experiment design, experimentation, ...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...
The Ku band radar system on the shuttle orbiter operates in both a search and a tracking mode, and i...
Stability and control, telecommunication system, solar array design, propellant feed system, and inf...
The results of the second phase of the Antenna Evaluation Study for the Shuttle Imaging Radar are pr...
Final results of the Spaceflight Tracking and Data Network (STDN) Ranging Equipment program are summ...
Simulated orbiter direct approaches during long duration exposure facility (LDEF) retrieval operatio...
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
A pre-entry communications study is presented for a relay link between a Jupiter entry probe and a s...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
Design of optomechanical system for remote oculometer for monitoring eye fixations without subject i...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
A project was conducted to extend the deployable antenna technology state-of-the art through the des...
Two state-of-the-art subsystems (detection and servo) were developed and performance generally more ...
The L-band positioning experiment is reported which encompassed experiment design, experimentation, ...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...
The Ku band radar system on the shuttle orbiter operates in both a search and a tracking mode, and i...
Stability and control, telecommunication system, solar array design, propellant feed system, and inf...
The results of the second phase of the Antenna Evaluation Study for the Shuttle Imaging Radar are pr...
Final results of the Spaceflight Tracking and Data Network (STDN) Ranging Equipment program are summ...
Simulated orbiter direct approaches during long duration exposure facility (LDEF) retrieval operatio...
Six scientific objectives/experiments were derived which consisted of agriculture/forestry/range res...
A pre-entry communications study is presented for a relay link between a Jupiter entry probe and a s...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
Design of optomechanical system for remote oculometer for monitoring eye fixations without subject i...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
A project was conducted to extend the deployable antenna technology state-of-the art through the des...
Two state-of-the-art subsystems (detection and servo) were developed and performance generally more ...
The L-band positioning experiment is reported which encompassed experiment design, experimentation, ...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...