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Book A Shadowgraph Study of the National Launch System s 1 1 2 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration

Download or read book A Shadowgraph Study of the National Launch System s 1 1 2 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration written by Darlene C. Pokora and published by . This book was released on 1994 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Shadowgraph Study of the National Launch System s 1 1

Download or read book A Shadowgraph Study of the National Launch System s 1 1 written by Darlene C. Pokora and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Shadowgraph Study of the National Launch System s 1 1 2 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration  Using the Marshall Space Flight Center s 14 Inch Trisonic Wind Tunnel

Download or read book A Shadowgraph Study of the National Launch System s 1 1 2 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration Using the Marshall Space Flight Center s 14 Inch Trisonic Wind Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: A shadowgraph study of the National Launch System's (NLS's) 1 1/2 stage and heavy lift launch vehicle (HLLV) configurations is presented. Shadowgraphs are shown for the range of Mach numbers from Mach 0.6 to 5.0 at various angles-of-attack and roll angles. Since the 1 1/2 stage configuration is generally symmetric, no shadowgraphs of any roll angle are shown for this configuration. The major flow field phenomena over the NLS 1 1/2 stage and HLLV configurations are shown in the shadowgraphs. These shadowgraphs are used in the aerothermodynamic analysis of the external flow conditions the launch vehicle would encounter during the ascent stage of flight. The shadowgraphs presented in this study were obtained from configurations tested in the Marshall Space Flight Center's 14-Inch Trisonic Wind Tunnel during 1992. Pokora, Darlene C. and Springer, Anthony M. Marshall Space Flight Center...

Book A Shadowgraph Study of the National Launch System s One and a half Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration

Download or read book A Shadowgraph Study of the National Launch System s One and a half Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration written by Darlene C. Pokora and published by . This book was released on 1994 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Shadowgraph Study of the National Launch System s 1   Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration

Download or read book A Shadowgraph Study of the National Launch System s 1 Stage Vehicle Configuration and Heavy Lift Launch Vehicle Configuration written by Darlene C. Pokora and published by . This book was released on 1994 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Shadowgraph Study of Space Transportation System  Sts

Download or read book A Shadowgraph Study of Space Transportation System Sts written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: A shadowgraph study of the space transportation system (STS), the space shuttle launch vehicle, is presented. The shadowgraphs presented in this study were obtained over the past 10 years from wind tunnel tests performed in the NASA Marshall Space Flight Center's 14-Inch Trisonic Wind Tunnel during the space shuttle development program. Shadowgraphs of the STS at various angles-of-attack and roll angles are shown for the Mach range of 0.6 to 4.96. The major flow field phenomena over the mated vehicle configuration are shown in these shadowgraphs. Shadowgraphs are also presented for the orbiter without the lower stack (reentry configuration) and the lower stack without the orbiter. A short study of external tank nose geometry effects on the mated vehicles flow field is presented. These shadowgraphs are used in the aerothermodynamic analysis of the external flow conditions the launch vehicle encounters during the ascent stage of flight. Springer, A. M. Langley Research Center...

Book Aerodynamic Characteristics of the National Launch System  NLS  1 1 2 Stage Launch Vehicle

Download or read book Aerodynamic Characteristics of the National Launch System NLS 1 1 2 Stage Launch Vehicle written by A. M. Springer and published by . This book was released on 1994 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalogue  United States Public Documents

Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1994-08 with total page 872 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Scientific and Technical Reports

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1966 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Selected Listing of NASA Scientific and Technical Reports for

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1965 with total page 1680 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Announcements   Index

Download or read book Government Reports Announcements Index written by and published by . This book was released on 1995 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Aeronautical Journal

Download or read book The Aeronautical Journal written by and published by . This book was released on 1994 with total page 472 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics of the National Launch System  Nls  1 1 2 Stage Launch Vehicle

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...