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Static Aerodynamic Characteristics Of A Model Of A Saturn 1 Block 2 Launch Vehicle With Proposed Spacecraft At Mach Numbers From 157 To 287
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Book Synopsis Static Aerodynamic Characteristics of a Model of a Saturn 1 Block 2 Launch Vehicle with Proposed Spacecraft at Mach Numbers from 1.57 to 2.87 by :
Download or read book Static Aerodynamic Characteristics of a Model of a Saturn 1 Block 2 Launch Vehicle with Proposed Spacecraft at Mach Numbers from 1.57 to 2.87 written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 by : Dennis E. Fuller
Download or read book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 40 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 of 0.016-scale Models of Two- and Three-stage Saturn Launch Vehicles with Conical and Winged Spacecraft at Mach Numbers from 1.57 to 4.65 by :
Download or read book Aerodynamic Characteristics of 0.016-scale Models of Two- and Three-stage Saturn Launch Vehicles with Conical and Winged Spacecraft at Mach Numbers from 1.57 to 4.65 written by and published by . This book was released on 1963 with total page 166 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 Transonic Aerodynamic Characteristics of a Saturn IB Manned Orbiting Research Laboratory Launch Vehicle by : Stuart G. Flechner
Download or read book Transonic Aerodynamic Characteristics of a Saturn IB Manned Orbiting Research Laboratory Launch Vehicle written by Stuart G. Flechner and published by . This book was released on 1969 with total page 52 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 An Aerodynamic Analysis of Saturn I, Block I Flight Test Vehicles by : Fernando S. Garcia
Download or read book An Aerodynamic Analysis of Saturn I, Block I Flight Test Vehicles written by Fernando S. Garcia and published by . This book was released on 1964 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several Proposd Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 by : Dennis E. Fuller
Download or read book Aerodynamic Characteristics of Several Proposd Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 32 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 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 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 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 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 Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° by : J. W. Usry
Download or read book Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° written by J. W. Usry and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1/10-scale Model of the Blue Scout Jr. at Mach Numbers from 0.40 to 1.03 by : Thomas C. Kelly
Download or read book Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1/10-scale Model of the Blue Scout Jr. at Mach Numbers from 0.40 to 1.03 written by Thomas C. Kelly and published by . This book was released on 1962 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781730724954 Total Pages :66 pages Book Rating :4.7/5 (249 download)
Book Synopsis Aerodynamic Characteristics of the National Launch System (Nls) 1 1/2 Stage Launch Vehicle by : National Aeronautics and Space Adm Nasa
Download or read book Aerodynamic Characteristics of the National Launch System (Nls) 1 1/2 Stage Launch Vehicle written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-02 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: The National Aeronautics and Space Administration (NASA) is studying ways of assuring more reliable and cost effective means to space. One launch system studied was the NLS which included the l l/2 stage vehicle. This document encompasses the aerodynamic characteristics of the 1 l/2 stage vehicle. To support the detailed configuration definition two wind tunnel tests were conducted in the NASA Marshall Space Flight Center's 14x14-Inch Trisonic Wind Tunnel during 1992. The tests were a static stability and a pressure test, each utilizing 0.004 scale models. The static stability test resulted in the forces and moments acting on the vehicle. The aerodynamics for the reference configuration with and without feedlines and an evaluation of three proposed engine shroud configurations were also determined. The pressure test resulted in pressure distributions over the reference vehicle with and without feedlines including the reference engine shrouds. These pressure distributions were integrated and balanced to the static stability coefficients resulting in distributed aerodynamic loads on the vehicle. The wind tunnel tests covered a Mach range of 0.60 to 4.96. These ascent flight aerodynamic characteristics provide the basis for trajectory and performance analysis, loads determination, and guidance and control evaluation. Springer, A. M. and Pokora, D. C. Marshall Space Flight Center...
