Author: John T. McSheraPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Aerodynamic Drag and Stability Characteristics of Towed Inflatable Decelerators at Supersonic Speeds
Author: John T. McSheraPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Aerodynamic Drag and Stability Characteristics of Towed Inflatable Decelerators at Supersonic Speeds
Author: John T. McSheraPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 0
Book Description
Results of a Free-flight Test to Determine the Performance Characteristics of a Towed, Conical Decelerator
Author: J. W. UsryPublisher:
ISBN:
Category : Results of a Free-Flight Test to Determine the Performance Characteristics of a Towed, Conical Decelerator
Languages : en
Pages : 48
Book Description
An inflatable fabric decelerator was tested in free flight to determine its drag and stability characteristics. The inflated decelerator approximated an 80 cone with a 48 inch (121.9) base and was towed behind a cone cylinder flare payload at a distance of 13.6 feet (4.15 m) from payload base.
NASA Technical Note
Author: Flow Field Survey and Decelerator Drag Characteristics in the Wake of a Model of the X-15 Airplane at Mach 2.30 and 4.65
Author: James F. CampbellPublisher:
ISBN:
Category : Acceleration (Mechanics)
Languages : en
Pages : 42
Book Description
Scientific and Technical Aerospace Reports
Author: A Selected Listing of NASA Scientific and Technical Reports for ...
Author: NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 260
Book Description
A Structural Merit Function for Aerodynamic Decelerators
Author: Melvin S. AndersonPublisher:
ISBN:
Category : Acceleration (Mechanics)
Languages : en
Pages : 44
Book Description
Structural merit function for aerodynamic decelerators.
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
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Acceleration (Mechanics)
Languages : en
Pages : 36
Book Description