Calorimetric evaluation of three 1.5-meter- diameter inflatable rigidized solar concentrators
Calorimetric evaluation of three 1.5-meter diameter inflatable rigidized solar concentrators for solar dynamic cycle power systems
Rhodes, M. D.↗
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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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Large-scale wind-tunnel investigation of an M1-L lifting body with an inflatable and a rigid afterbody
Large scale wind tunnel investigation of lifting body with inflatable and rigid afterbody
Falarski, M. D.↗
Effect of small bending stiffness on deformation of inflated structures.
Small bending stiffness effect on inflated torus and cylindrical shells under radial load for determining large space structure stiffness
Jordan, P. F.↗
Inflatable solar shields for cryogenic space vehicles.
Inflatable solar shields for thermal protection of space vehicles utilizing cryogen propellants
Jones, L. R.↗
Development status of attached inflatable decelerators.
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Bohon, H. L.↗
Experimental results of the deployment/rapid inflation characteristics 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.↗
Adequacy of the passive inflated falling sphere technique
Inflated falling sphere for high altitude sounding at radar site
Mc Watters, K. D.↗
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.↗
Determination of inflated shape and inertial properties of an all-flexible parawing
Determination of inflated shape and inertial properties of all-flexible parawing
Gloss, B. B.↗
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.↗
Inflatable honeycomb Patent
Inflatable honeycomb panel element for lightweight structures usable in space stations and other construction
Schnitzer, E.↗
Inflatable radar reflector unit Patent
Inflatable radar reflector unit - lightweight, highly reflective to electromagnetic radiation, and adaptable for erection and deployment with minimum effort and time
Radnofsky, M. I.↗
Thermal testing of inflatable solar shields for cryogenic space vehicles
Thermal testing of inflatable solar shields for cryogenic space vehicles, discussing shield misalignment effects on propellant tank temperatures
Doughty, R. O.↗
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.↗
Magnetosphere inflation during four magnetic storms in 1965
Magnetic storms development via initial asymmetric inflation of evening magnetosphere, using Explorer 26 and ground observatory data
Cahill, L. J., Jr.↗
Attached Inflatable Decelerator performance evaluation and mission-application study
Attached Inflatable Decelerator for planetary atmospheric entry, discussing mission applications and wind tunnel models performance
Bohon, H. L.↗
Structural behavior of tapered inflated fabric cylinders under various loading conditions
Method analyzes inflatable structures and considers axial loads, torsional moment, and internal pressure. Behavior depends on anistropic nature and large deflection stress-strain characteristics of fabric material. Behavior equations for pressurized cylinder loaded in torsion are developed.
Kovalevsky, L.↗
Inflation system for balloon type satellites Patent
Inflation system for balloon type satellites
Chapman, R. M.↗