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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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Inflatable tourniquet effects on cardiovascular deconditioning during bed rest and water immersion studies on humans
Inflatable conical shell afterbody ballute for aerodynamic brakes in Mars atmospheric entry
Magnetic dipole nonlinear inflation by plasma explained by gas pressure noting relevance to geomagnetic storms
Mechanics of inflatable sandwich type shallow shells
Heat transfer from inflatable spherical balloon shadow shield to spherical cryogen storage tank, noting several design factors and extensions of previous work
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Inflatable shell of revolution subject to asymmetric in-service loads noting field equations, mathematical model and numerical integration
Inflatable bladder facilitates the removal of heavy, highly finished metal parts from tote boxes or shipping containers. The proposed concept permits removal without danger of damage to the parts or injury to handling personnel.
Analysis of inflatable landing systems - Mars soft lander capsule study
Wind tunnel tests of inflatable disk-gap-band and modified ringsail parachutes at low dynamic pressure
Inflatable landing system investigated for impact normal to smooth surface
Calorimetric evaluation of three 1.5-meter diameter inflatable rigidized solar concentrators for solar dynamic cycle power systems
Large scale wind tunnel investigation of lifting body with inflatable and rigid afterbody
Small bending stiffness effect on inflated torus and cylindrical shells under radial load for determining large space structure stiffness
Inflatable solar shields for thermal protection of space vehicles utilizing cryogen propellants
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Buoyant Venus Station balloon for deployment and inflation during parachute descent into Venus atmosphere tested with scale model balloons in wind tunnels
Inflated falling sphere for high altitude sounding at radar site