Investigation of the reliability of a proposed confidence level procedure for error probability of a bank of correlators
Reliability of proposed confidence level procedure for error probability of bank of correlations
ERROR FUNCTION↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A discussion of proposed landing sites for AAP lunar missions
Proposed landing sites for Apollo applications program lunar missions
LANDING SITE↗
Nondestructive testing for space applications. Feasibility and preliminary design study. Part 3 - Proposed flight hardware program Final report
Feasibility of nondestructive testing in space environment - proposed flight hardware for prototype nondestructive test unit
Zoran, W. A.↗
Retrodirective antennas and the multipath problems associated with their use on the proposed orbiting data relay network
Retrodirective antennas and multipath transmission problems associated with use on proposed orbiting data relay network
Seal, P. M.↗
A proposed test of the Einstein theory of gravitation by means of an unshielded orbiting gyro using passive telemetry
Proposed test of theory of gravitation by an unshielded earth orbiting gyroscope using passive telemetry
Cooper, D. H.↗
A study of two proposed stabilization techniques for the X-15 horizontal surface control system
Two proposed stabilization methods for X-15 horizontal surface control system
Deazley, W. R.↗
Proposed technique for vertical alignment of a crane's cable
Proposed vertical alignment technique senses the attitude of a cranes cable and displays any deviation from the vertical. The system consists of a detector assembly fixed to the boom and a display scope located in the cabin. It has potential application with either fixed-boom cranes or gantries.
Gera, J., Jr.↗
The Goddard Space Flight Center cosmic dust experiment proposal for Pioneer F and G
Cosmic dust experiment proposal for Pioneer F-G
Berg, O. E.↗
Study of improved parts control technology for advanced planetary missions. Volume 3 - Text of proposed contractual requirements
Proposed contractual requirements to implement ultrahigh-reliability of parts for advanced planetary missions
Source record↗
Comments on viscoelastic transitions and the proposed liquid-liquid transition in polystyrene
Viscoelastic transitions and proposed liquid- liquid transition in polystyrene
Plazek, D. J.↗
Differences between proposed Apollo sites. I - Synthesis.
Spectral reflectivity and emissivity observations of proposed Apollo landing sites compared with other lunar localities and unmanned lunar probe data
Goetz, A. F. H.↗
Differences between proposed Apollo sites. III - Far infrared emissivity evidence.
Lunar surface IR emissivity comparison spectra including proposed Apollo landing sites, indicating Si-O ratio difference for Plato crater
Goetz, A. F. H.↗
A method for more efficient use of the 4B voice/data lines with application to the proposed AAP teleprinter
Use of 4B voice/data lines with application to proposed AAP teleprinter
Dotson, W. P., Jr.↗
A proposal concerning terminology in reduced density matrix theory
Proposed terminology for reduced density matrix theory
Harriman, J. E.↗
Evaluation of the LM guidance system performance over the approach terrain of five of the proposed Apollo landing sites - Apollo program
Evaluation of lunar module guidance system performance over approach terrain of five proposed Apollo landing sites
Dyer, D. A.↗
Hypervelocity impact tests on a proposed lunar tug fuel tank configuration
Hypervelocity impact tests to predict meteoritic damage on proposed lunar tug fuel tank configuration
Jex, D. W.↗
The effect of mission attitude timelines on consumables requirements for the proposed shuttle orbiter heat rejection systems
Effect of mission attitude timelines on consumables requirements for proposed shuttle orbiter heat rejection systems
Cunningham, J. E.↗
Proposed techniques for launching instrumented balloons into tornadoes
A method is proposed to introduce instrumented balloons into tornadoes by means of the radial pressure gradient, which supplies a buoyancy force driving to the center. Presented are analytical expressions, verified by computer calculations, which show the possibility of introducing instrumented balloons into tornadoes at or below the cloud base. The times required to reach the center are small enough that a large fraction of tornadoes are suitable for the technique. An experimental procedure is outlined in which a research airplane puts an instrumented, self-inflating balloon on the track ahead of the tornado. The uninflated balloon waits until the tornado closes to, typically, 750 meters; then it quickly inflates and spirals up and into the core, taking roughly 3 minutes. Since the drive to the center is automatically produced by the radial pressure gradient, a proper launch radius is the only guidance requirement.
Grant, F. C.↗