Performance of a towed, 48-inch-diameter /121.92-cm/ ballute decelerator tested in free flight at Mach numbers from 4.2 to 0.4
Inflation, drag, and stability characteristics of towed inflatable ballute decelerator at free flight
Usry, J. W.↗
SEARCH · Search NASA
Results for “decelerators”
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.
Dynamics of towed decelerators
Two body mathematical model for flexible tow line- decelerator dynamical system
Campbell, J. F.↗
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.↗
Static longitudinal aerodynamic characteristics of some supersonic decelerator models at Mach numbers of 2.30 and 4.63
Aerodynamic characteristics of blunted cones, tension shell, and attached inflatable decelerator models
Davenport, E. E.↗
Results of a free-flight test to determine the performance characteristics of a towed, conical decelerator
Drag and stability characteristics of towed, conical decelerator
Usry, J. W.↗
Deceleration-control system for aerobraking and skipout to orbit at Mars.
Deceleration control system for aerobraking and skipout to orbit at Mars
Schy, A. A.↗
Evaluation of entry and terminal deceleration systems for unmanned Martian landers.
Entry and terminal deceleration systems for unmanned Martian landers, discussing parachute landing and lifting entry vehicles
Harrison, E. F.↗
Development status of attached inflatable decelerators.
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Bohon, H. L.↗
Deceleration control system for aerobraking and skipout to orbit at Mars.
Deceleration control system for aerobraking and skipout to orbit at Mars
Schy, A. A.↗
Deployable aerodynamic decelerators for space missions.
Aerodynamic deceleration systems for space missions, considering deployment of subsonic parachute and inflatable configuration following atmospheric entry
Gillis, C. L.↗
Limits on the cosmological deceleration parameter.
Deceleration parameter lower and upper limits for zero pressure big bang cosmological Friedmann models imposed by density parameter, Hubble constant and universe age
Rindler, W.↗
Status of research on parawing lifting decelerators.
Flexible parawing lifting decelerator research data from wind tunnel and flight tests, noting manned space vehicle recovery and aircraft escape systems
Gainer, T. G.↗
A structural merit function for aerodynamic decelerators
Structural merit function for aerodynamic decelerators
Anderson, M. S.↗
Controlled deceleration specimen protection systems for electrodynamic vibration systems
Controlled deceleration specimen protection systems for electrodynamic vibration systems
Cook, L. L., Jr.↗
Wake analysis for supersonic decelerator applications. Volume 2 - Application of gas-hydraulic analogy to shallow-water tow channel results
Shallow water tow channel used to study two dimensional compressible wake of supersonic decelerator
Lau, R. A.↗
Drag characteristics of several towed decelerator models at Mach 3
Drag characteristics of toroid-membrane and wide-angle conical shells used as towed decelerators
Bohon, H. L.↗
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.↗
Annular supersonic decelerator or drogue Patent
Bluff-shaped annular configuration for supersonic decelerator for reentry vehicles
Connors, J. F.↗