Author: Roger H. FournierPublisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Supersonic Aerodynamic Characteristics of a Saturn IB Launch Vehicle Model with Third-stage Modifications
Author: Roger H. FournierPublisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1282
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65
Author: Dennis E. FullerPublisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 40
Book Description
Government-wide Index to Federal Research & Development Reports
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1466
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2300
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2088
Book Description
A Supersonic/hypersonic Aerodynamic Investigation of the Saturn IB/Apollo Upper Stage
Author: David R. CarlsonPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 76
Book Description
The static stability and axial force characteristics of an upper stage Saturn IB/Apollo model were investigated in a series of wind tunnel tests at Mach numbers between 1.93 and 8.05. This report presents and analyzes the results of these small scale studies. Test procedures and models are described, and consideration of boundary layer characteristics and violated modeling rules yields an assessment of the validity of the data Four basic models provided evaluation of the basic launch vehicle characteristics, as well as the effects of two modes of mission abort and jettison of the launch escape system. The launch configuration experienced sudden, strong changes in stability derivatives and axial force coefficients near Mach 5. No similar changes were observed on the other configurations. Effects of Reynolds number, Mach number, and boundary layer trips were obtained for each shape. The faired curves are believed to be valid for full-scale flight of the Saturn IB/Apollo upper stage.
U.S. Government Research & Development Reports
Author: NASA SP.
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1090
Book Description
A Selected Listing of NASA Scientific and Technical Reports for 1966
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2084
Book Description
