Author: Edward L. Hoffman
Publisher:
ISBN:
Category : Parachutes
Languages : en
Pages : 38
Book Description
Effect of a Load-alleviating Structure on the Landing Behavior of a Reentry-capsule Model
Author: Edward L. Hoffman
Publisher:
ISBN:
Category : Parachutes
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Parachutes
Languages : en
Pages : 38
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
NASA Technical Note
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1274
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1274
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1284
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1284
Book Description
Space Rendez[v]ous, Rescue and Recovery
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 128
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 128
Book Description
Bibliography of Scientific and Industrial Reports
Landing Characteristics of the Apollo Spacecraft with Deployed-heat-shield Impact Attenuation Systems
Author: Sandy M. Stubbs
Publisher:
ISBN:
Category : Shielding (Heat)
Languages : en
Pages : 64
Book Description
An experimental investigation was made to determine the landing characteristics of a 1/4-scale dynamic model of the Apollo spacecraft command module using two different active (heat shield deployed prior to landing) landing systems for impact attenuation. One landing system (configuration 1) consisted of six hydraulic struts and eight crushable honeycomb struts. The other landing system (configuration 2), consisting of four hydraulic struts and six strain straps, was lighter. Tests made on water and the hard clay-gravel composite landing surfaces simulated parachute letdown (vertical) velocities of 23 ft/sec (7.0 m/s) (full scale). Landings made on the sand landing surface simulated vertical velocities of 30 ft/sec (9.1 m/s). Horizontal velocities of from 0 to 50 ft/sec (15 m/s) were simulated. Landing attitudes ranged from -30 degrees to 20 degrees , and the roll attitudes were 0 degrees, 90 degrees, and 180 degrees.
Publisher:
ISBN:
Category : Shielding (Heat)
Languages : en
Pages : 64
Book Description
An experimental investigation was made to determine the landing characteristics of a 1/4-scale dynamic model of the Apollo spacecraft command module using two different active (heat shield deployed prior to landing) landing systems for impact attenuation. One landing system (configuration 1) consisted of six hydraulic struts and eight crushable honeycomb struts. The other landing system (configuration 2), consisting of four hydraulic struts and six strain straps, was lighter. Tests made on water and the hard clay-gravel composite landing surfaces simulated parachute letdown (vertical) velocities of 23 ft/sec (7.0 m/s) (full scale). Landings made on the sand landing surface simulated vertical velocities of 30 ft/sec (9.1 m/s). Horizontal velocities of from 0 to 50 ft/sec (15 m/s) were simulated. Landing attitudes ranged from -30 degrees to 20 degrees , and the roll attitudes were 0 degrees, 90 degrees, and 180 degrees.