RAE antenna-damper package deployment interaction
Deflections of RAE spacecraft antennas caused by transient disturbance associated with deployment of damper package
Fedor, J. V.↗
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Results for “deployables”
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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Techniques for selection and analysis of parachute deployment systems
Equations of motion for parachute deployment analysis
Huckins, E. K., III↗
Some thoughts on gearhead electric motors for spacecraft boom deployment mechanisms
Gearhead electric motor choices for spacecraft boom deployment applications
Mac Naughton, J.↗
A deployment fixture for the simulated zero- gravity testing of a large-area solar array
Design and development of deployment fixture for simulated zero gravity testing of large area solar array
James A Lackey↗
Dynamic analysis of stability and deployment of inflatable shell structures Final report
Dynamic analysis of stability and deployment of inflatable shell structures for space vehicle antennas and gravity-gradient damper booms
Falgout, T. E.↗
Investigation of the aerodynamic characteristics and wing-deployment transients of the NASA DL-4 body with a sailwing landing aid Final report
Aerodynamic characteristics and wing deployment transients of NASA DL-4 lifting body fitted with sailwing landing aid
Bohn, J.↗
Performance and deployment characteristics of a twin-keel parawing with various amounts and permeabilities of porous material in outer lobes
Performance and deployment characteristics of twin-keel parawing with different amounts and permeabilities of porous material in outer lobes
Morgan, H. L., Jr.↗
High-altitude flight test of a 40-foot- diameter /12.2-meter/ ringsail parachute at a deployment Mach number of 2.95
High altitude flight test of ringsail parachute with deployment at Mach 2.95
Eckstrom, C. V.↗
Radiation pattern calculations for an ATS-F 48-panel deployable-reflector antenna
Radiation pattern calculations for ATS 6 48-panel deployable reflector antenna
Miezis, R.↗
Deployment and performance characteristics of 5-foot diameter /1.5 m/ attached inflatable decelerators from Mach number 2.2 to 4.4
Deployment and steady state performance of supersonic attached inflatable decelerator canopy models
Bohon, H. L.↗
Wing deployment method and apparatus Patent
Method for deployment of flexible wing glider from space vehicle with minimum impact and loading
Sutliff, J. D.↗
Flexible wing deployment device Patent
Deployment system for flexible wing with rigid superstructure
Libbey, C. E.↗
Deployment techniques developed for large area roll-out solar arrays
Deployment systems for extending large area lightweight flexible solar arrays in space, tabulating estimated design weights including power-weight ratios
Hasbach, W. A.↗
Thermal analysis of the 14-foot deployable parabolic antenna
Thermal analysis of deployable parabolic antenna for Outer Planetary Explorer program, discussing spacecraft spin and radioisotope thermoelectric generators effect
Kay, S.↗
Orbital deployment of very long tethered structures
Earth-pointing satellites joined by tether, discussing reel back and drag brake orbital deployment techniques and dynamic behavior
Bush, G. B.↗
Deployment and inflation characteristics tests of a Buoyant Venus Station balloon
Buoyant Venus station balloon for deployment and inflation during parachute descent into Venus atmosphere tested with scale model balloons in wind tunnels
Holle, G. F.↗
Some analysis of parawing canopy behavior during free flight deployment
Parawing canopy behavior during deployment in free flight at specific altitudes and dynamic pressures
Clemmons, D. L., Jr.↗