Simulation of deployment dynamics of spinning spacecraft.
Simulation of deployment dynamics of spinning spacecraft, discussing test methods emphasizing gravity compensating techniques
DYNAMICS↗
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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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A method for calculating parachute opening forces for general deployment conditions.
Calculating method for parachute opening forces, system velocity, cloth pressure loading and filling time for horizontal and vertical deployment conditions
NUMERICAL INTEGRATION↗
Deployable lattice column
Lattice column, made up of many individually collapsible sections connected in tandem, rapidly raises measuring instruments to a level appreciably above that where data is to be recorded and evaluated. The column may be collapsed by collapsing each section in sequence and is deployed by extending each section in sequence.
Mauch, H. R.↗
Flight test of a 15-foot-diameter /4.6-meter/ 120 deg conical spacecraft simulating parachute deployment in a Mars atmosphere
Flight test of conical spacecraft simulating parachute deployment in Mars atmosphere
Darnell, W. L.↗
Water pressure and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module with deployed heat shield impact attenuation system
Stubbs, S. M.↗
Deployable large area solar cell array testing Quarterly report
Detail design, acceleration and vacuum tests, and support fixtures for deployable solar array
Source record↗
Flight test of a 40-foot nominal diameter disk gap band parachute deployed at a Mach number of 1.91 and a dynamic pressure of 11.6 pounds per square foot
Flight test of l0-foot nominal-diameter disk-gap band parachute to determine deployment and inflation, opening shock loads, drag efficiency, and stability characteristics
Eckstrom, C. V.↗
Feasibility development of a self-deploying electromagnetic energy focusing reflector for space or transportable ground based applications
Feasibility development of self-deploying electromagnetic energy focusing reflector for space or transportable ground based operations
Bahiman, H.↗
Flight test of a 40-foot-nominal-diameter disk-gap-band parachute deployed at a Mach number of 2.72 and a dynamic pressure of 9.7 pounds per square foot
Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressure
Eckstrom, C. V.↗
Free-flight and wind-tunnel studies of deployment of a dynamically and elastically scaled inflatable parawing model
Deployment characteristics of dynamic and elastic parawing scale model for spacecraft recovery
Ferris, A. T.↗
Full-scale simulation of parachute deployment environment in the atmosphere of Mars
Simulation of parachute deployment environment in Mars atmosphere
Bendura, R. J.↗
A method for controlling parachute deployment conditions in simulated planetary environments
Controlling parachute deployment conditions in simulated planetary environments
Murrow, H. N.↗
A method for controlling parachute deployment conditions in simulated planetary environments.
NASA Planetary Entry Parachute Program /PEPP/, discussing method to control parachute deployment conditions in simulated planetary environments by radio command system
Murrow, H. N.↗
Deployment of spacecraft appendages and temperature control of experiments Final technical report
Deployment dynamics and temperature control of spacecraft solar panel array and X ray telescope
Blanton, R. W., Jr.↗
Mechanisms for restraining and deploying a 50-kW solar array
Design and hardware of restraining and deploying mechanism for solar array of Mars flyby mission
Haynie, T.↗
Deployable large area solar cell array testing
Large area deployable solar cell array testing
Source record↗
Positive deployable solar array development program - phase 3 Final report
Design and flight certification test data on prototype deployable solar cell array
Source record↗
Flight-test results from supersonic deployment of an 18-foot-diameter /5.49 meter/ towed ballute decelerator
Supersonic deployment and extraction of inflatable towed ballute decelerator
Eckstrom, C. V.↗