Structural analysis of a parawing during deployment
Finite element analysis of critical stress distribution in canopy of deployed twin keel parawing, predicting failure stress levels
Kenner, P. M.↗
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
A new technique for predicting the snatch force generated during lines-first deployment of an aerodynamic decelerator
Snatch force during lines-first deployment of aerodynamic decelerator, including effects of canopy skirt acceleration and suspension wave propagation characteristics
Huckins, E. K., III↗
Dynamics of a large spin-stiffened deployable paraboloidal antenna
Dynamics of deployable space structures stiffened by centrifugal forces due to spin, discussing LF radio telescope
Hedgepeth, J. M.↗
Optimization of RAE satellite boom deployment timing
Radio Astronomy Explorer satellite boom deployment method resulting in gravity gradient capture, emphasizing role of predeployment attitude and antenna Vee angle
Bowers, E. J., Jr.↗
Automatically deploying nozzle exit cone extension Patent
Automatically deploying nozzle exit cone extension
Ward, D. R.↗
A computer program to study the motion and appendage stresses of a satellite deploying a number of asymmetrical segmented appendages /N-boom/, users manual, volume 1 Final report
Computer program for predicting motion and appendage stresses of spacecraft during deployment maneuvers
Grote, P. B.↗
Method for estimating minimum required ejection velocity for parachute deployment
Approximate method for estimating minimum required ejection velocity for parachute deployment
Huckins, E. K., III↗
Radiator deployment actuator Patent
Hydraulic actuator design for space deployment of heat radiators
Kolstee, H. M.↗
Flight tests of cross, modified ringsail, and disk-gap-band parachutes from a deployment altitude of 3.05 km /10,000 ft/
Flight tests of cross, modified ringsail, and disk-gap-band parachute deployment performance from low altitudes with structural load data
Eckstrom, C. V.↗
Aerodynamic and deployment characteristics of multistage canopy and suspension-line reefing systems for a twin-keel all-flexible parawing
Aerodynamic and deployment characteristics of twin keel all-flexible parawing rigged with several variations of multistage canopy and suspension line reefing system
Mc Hatton, A. D.↗
Deployable aerodynamic decelaration systems - Space vehicle design criteria
Criteria and recommended practices for design, selection, analysis, and testing of deployable aerodynamic deceleration systems
Source record↗
Geometric, aerodynamic, and kinematic characteristics of two twin keel parawings during deployment
Flight test data on geometric, aerodynamic, and kinematic characteristics of two twin keel parawings during deployment
Churchill, F. T.↗
Deployment loads data from a free flight investigation of all-flexible parawings at small scale
Determining deployment characteristics of all-flexible parawings by free flight tests
Croom, D. R.↗
High-Altitude Flight Test of a Reefed 12.2-Meter-Diameter Disk-Gap-Band Parachute with Deployment at a Mach Number of 2.58
High altitude flight test of reefed 12.2-meter-diameter disk-gap-band parachute with deployment at 2.58 Mach number
Preisser, J. S.↗
A study of wire-deploying devices designed to trigger lightning
Development and characteristics of device for deployment of long wires as method of reducing hazards due to lightning during spacecraft launches
Rossow, V. J.↗
Exploratory wind-tunnel investigation of deployable flexible ventral fins for use as an emergency spin-recovery device
Spin tunnel tests to determine effectiveness of deployable, flexible ventral fins for spin recovery device on fighter aircraft
Burk, S. M., Jr.↗
Snatch force during lines-first parachute deployments
Snatch force during lines-first deployment of aerodynamic decelerator, including effects of canopy skirt acceleration and suspension wave propagation characteristics
Huckins, E. K., III↗
Self-deploying boom
Development and operation of metal ribbon which acts like self deploying boom are described. Metal ribbon is retained on two rollers for storage and extends into nonretractable tubular structure upon release. Illustration of equipment is provided.
Tumulty, W. T.↗