Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot /

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Techniques for selection and analysis of parachute deployment systems /

Huckins, Earle K., 1943-
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

Penetration of drops into high-velocity airstreams /

Ingebo, Robert D.
Lewis Research Center.

January 1967

"NASA TM X-1363.""Lewis Research Center, Cleveland, Ohio.""April 1967"--Cover.Includes bibliographic...

Flight test of a 15-foot-diameter (4.6-meter) 120 ̊conical spacecraft simulating parachute deployment in a Mars atmosphere /

Darnell, Wayne L.
Lundstrom, Reginald R.
Henning, Allen B.
Langley Research Center.

Prepared at Langley Research Center."December 1967"--Cover.Includes bibliographical references (p. 2...

Performance of a 26-meter-diameter ringsail parachute in a simulated Martian environment /

Whitlock, Charles H.
Coltrane, Lucille C.
Bendura, Richard J.
Langley Research Center.

January 1967

"NASA TM X-1356.""Langley Research Center, Langley Station, Hampton, Va.""March 1967"--Cover.Include...

Wind-tunnel tests of modified cross, hemisflo, and disk-gap-band parachutes with emphasis in the transonic range /

Foughner, James T.
Alexander, William C. (William Campbell)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Flight test of a 31.2-foot-diameter modified ringsail parachute deployed at a Mach number of 1.39 and a dynamic pressure of 11.0 pounds per square foot /

Preisser, John S.
Murrow, Harold N.
Eckstrom, Clinton V.
Langley Research Center.

January 1967

"Technical film supplement L-966 available on request.""August 1967."Includes bibliographical refere...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Flight Test of a 30-Foot Nominal-Diameter Disk-Gap-Band Parachute Deployed at Mach 1.56 and Dynamic Pressure of 11.4 Pounds per Square Foot

Eckstrom, Clinton V.
Preisser, John S.

September 1967

A 30-foot (9.1 meter) nominal-diameter disk-gap-band parachute (reference area 707 sq ft (65.7 m(exp...

High-altitude flight test of a reefed 12.2-meter-diameter disk-gap-band parachute with deployment at a mach number of 2.58 /

Preisser, John S.
Grow, R. Bruce.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...

Flight tests of Viking parachute system in three Mach number regimes /

Lundstrom, Reginald R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references.1. Vehicle descr...

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

Preisser, J. S.
Eckstrom, C. V.

August 1968

Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressur

Experimental determination of the apparent moment of inertia of parachutes /

Ibrahim, Shukry K., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
University of Minnesota. Department of Aerospace Engineering and Mechanics. sponsor.

"April 1965."Includes bibliograpical references (pages 43).Air Force Contract No.Mode of access: Int...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Techniques for selection and analysis of parachute deployment systems /

Huckins, Earle K., 1943-
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

Penetration of drops into high-velocity airstreams /

Ingebo, Robert D.
Lewis Research Center.

January 1967

"NASA TM X-1363.""Lewis Research Center, Cleveland, Ohio.""April 1967"--Cover.Includes bibliographic...

Flight test of a 15-foot-diameter (4.6-meter) 120 ̊conical spacecraft simulating parachute deployment in a Mars atmosphere /

Darnell, Wayne L.
Lundstrom, Reginald R.
Henning, Allen B.
Langley Research Center.

Prepared at Langley Research Center."December 1967"--Cover.Includes bibliographical references (p. 2...

Performance of a 26-meter-diameter ringsail parachute in a simulated Martian environment /

Whitlock, Charles H.
Coltrane, Lucille C.
Bendura, Richard J.
Langley Research Center.

January 1967

"NASA TM X-1356.""Langley Research Center, Langley Station, Hampton, Va.""March 1967"--Cover.Include...

Wind-tunnel tests of modified cross, hemisflo, and disk-gap-band parachutes with emphasis in the transonic range /

Foughner, James T.
Alexander, William C. (William Campbell)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Flight test of a 31.2-foot-diameter modified ringsail parachute deployed at a Mach number of 1.39 and a dynamic pressure of 11.0 pounds per square foot /

Preisser, John S.
Murrow, Harold N.
Eckstrom, Clinton V.
Langley Research Center.

January 1967

"Technical film supplement L-966 available on request.""August 1967."Includes bibliographical refere...

Wind-tunnel tests of a series of 18-foot-diameter parachutes with extendable flaps /

Gamse, Berl.
Yaggy, Paul F.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Aerodynamics, missiles and space vehicles; Atmospheric entry.Includes bibl...

Flight Test of a 30-Foot Nominal-Diameter Disk-Gap-Band Parachute Deployed at Mach 1.56 and Dynamic Pressure of 11.4 Pounds per Square Foot

Eckstrom, Clinton V.
Preisser, John S.

September 1967

A 30-foot (9.1 meter) nominal-diameter disk-gap-band parachute (reference area 707 sq ft (65.7 m(exp...

High-altitude flight test of a reefed 12.2-meter-diameter disk-gap-band parachute with deployment at a mach number of 2.58 /

Preisser, John S.
Grow, R. Bruce.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

A reefed B.2-meter nominal-diameter (40-ft) disk-gap-band parachute was flight tested as part of the...

Flight tests of Viking parachute system in three Mach number regimes /

Lundstrom, Reginald R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references.1. Vehicle descr...

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

Preisser, J. S.
Eckstrom, C. V.

August 1968

Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressur

Experimental determination of the apparent moment of inertia of parachutes /

Ibrahim, Shukry K., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
University of Minnesota. Department of Aerospace Engineering and Mechanics. sponsor.

"April 1965."Includes bibliograpical references (pages 43).Air Force Contract No.Mode of access: Int...

Flight measurements of surface pressures on a flexible supercritical research wing /

Eckstrom, Clinton V.
Langley Research Center.

January 1985

Prepared at Langley Research Center."December 1985"--Cover.Includes bibliographical references (p. 1...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraft /

Bugg, Frank M.
Sleeman, William C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."June 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Techniques for selection and analysis of parachute deployment systems /

Huckins, Earle K., 1943-
Langley Research Center.

Prepared at Langley Research Center."January 1970."Cover title.Includes bibliographical references (...

Penetration of drops into high-velocity airstreams /

Ingebo, Robert D.
Lewis Research Center.

January 1967

"NASA TM X-1363.""Lewis Research Center, Cleveland, Ohio.""April 1967"--Cover.Includes bibliographic...

Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot /

Abstract

Extracted data

Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot /

Abstract

Extracted data

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