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Static Longitudinal Aerodynamic Characteristics Of A Powered Model Of The Apollo Launch Escape Vehicle From Mach 050 To 130
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Book Synopsis Static Longitudinal Aerodynamic Characteristics of a Powered Model of the Apollo Launch-escape Vehicle from Mach 0.50 to 1.30 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a Powered Model of the Apollo Launch-escape Vehicle from Mach 0.50 to 1.30 written by and published by . This book was released on 1966 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65 by : Robert H. Moore
Download or read book Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65 written by Robert H. Moore and published by . This book was released on 1968 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a 0.028 Scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 1.50 to 2.16 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a 0.028 Scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 1.50 to 2.16 written by and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a Model of a Two-stage Version of a Saturn Launch Vehicle with a Proposed Apollo Payload at Mach Numbers from 1.57 to 2.87 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a Model of a Two-stage Version of a Saturn Launch Vehicle with a Proposed Apollo Payload at Mach Numbers from 1.57 to 2.87 written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics Determined During Development of the Apollo Launch Escape Vehicle Configuration by : William C. Moseley (Jr.)
Download or read book Aerodynamic Characteristics Determined During Development of the Apollo Launch Escape Vehicle Configuration written by William C. Moseley (Jr.) and published by . This book was released on 1969 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a 0.028-scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 0.50 to 1.20 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a 0.028-scale Model of a Proposed Little Joe-Apollo Space Vehicle at Mach Numbers from 0.50 to 1.20 written by and published by . This book was released on 1962 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle by : William C. Moseley (Jr.)
Download or read book Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle written by William C. Moseley (Jr.) and published by . This book was released on 1967 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of Powered Models of Several Apollo Launch-escape Vehicle Configurations by : Bobby L. Berrier
Download or read book Transonic Aerodynamic Characteristics of Powered Models of Several Apollo Launch-escape Vehicle Configurations written by Bobby L. Berrier and published by . This book was released on 1968 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Configurations of a Proposed Little Joe 2-Apollo Space Vehicle at Mach Numbers from 0.30 to 1.20 by :
Download or read book Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Configurations of a Proposed Little Joe 2-Apollo Space Vehicle at Mach Numbers from 0.30 to 1.20 written by and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Static Longitudinal Aerodynamic Characteristics at Angles of Attack from Minus 2 Deg to 95 Deg of a Proposed Little Joe 2-apollo Space Vehicle by :
Download or read book Subsonic Static Longitudinal Aerodynamic Characteristics at Angles of Attack from Minus 2 Deg to 95 Deg of a Proposed Little Joe 2-apollo Space Vehicle written by and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of a 0.07-scale Model of a Proposed Apollo Spacecraft at Mach Numbers of 1.57 to 4.65 by :
Download or read book Static Longitudinal Aerodynamic Characteristics of a 0.07-scale Model of a Proposed Apollo Spacecraft at Mach Numbers of 1.57 to 4.65 written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a 0.030-scale Model of a Little Joe 2-Apollo Space Vehicle at Mach Numbers from 1.57 to 4.65 by :
Download or read book Static Stability and Control Characteristics of a 0.030-scale Model of a Little Joe 2-Apollo Space Vehicle at Mach Numbers from 1.57 to 4.65 written by and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Models of Reentry and Atmospheric-abort Configurations of a Proposed Apollo Spacecraft at Mach Numbers from 0.30 to 1.20 by :
Download or read book Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Models of Reentry and Atmospheric-abort Configurations of a Proposed Apollo Spacecraft at Mach Numbers from 0.30 to 1.20 written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle with Low Planform Loading at Mach Numbers from 0.3 to 4.63 by : Delma C. Freeman
Download or read book Static Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle with Low Planform Loading at Mach Numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1977 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65 by : Robert H. Moore
Download or read book Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II-Apollo Test Vehicle at Mach Numbers from 0.056 to 4.65 written by Robert H. Moore and published by . This book was released on 1968 with total page 213 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 by :
Download or read book Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of a Modified Model of a Proposed Apollo Atmospheric Abort Configuration at Mach Numbers from 0.30 to 1.20 by : Albin O. Pearson
Download or read book Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of a Modified Model of a Proposed Apollo Atmospheric Abort Configuration at Mach Numbers from 0.30 to 1.20 written by Albin O. Pearson and published by . This book was released on 1962 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
