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Book Aerodynamic Characteristics of Two Single Stage To Orbit Vehicles at Mach 20 3

Download or read book Aerodynamic Characteristics of Two Single Stage To Orbit Vehicles at Mach 20 3 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The hypersonic stability, control, and performance characteristics of two configurations have been determined. Each configuration had a 50 deg swept delta wing, a vertical tail, and a body flap. One model represented a control configured vehicle with a reduced level of longitudinal static stability; the other model was designed for a conventional level of stability. Data were obtained over an angle of attack range of 0 deg to 50 deg and included effects of component buildup. In addition, the effects of the vertical tail on the lateral directional characteristics were obtained. Bernot, P. T. Langley Research Center NASA-TM-X-3550, L-11627 RTOP 506-26-10-08...

Book Static Aerodynamic Characteristics of a Single stage to orbit Vehicle with Low Planform Loading at Mach Numbers from 0 3 to 4 63

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 Static Aerodynamic Characteristics of a Single stage to orbit Vehicle with Low Planform Loading at Mach Numbers from 0 3 to 4 63

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 Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1 57 to 4 65

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 Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1973 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Transonic Aerodynamic Characteristics of a Proposed Wing Body Reusable Launch Vehicle Concept

Download or read book Transonic Aerodynamic Characteristics of a Proposed Wing Body Reusable Launch Vehicle Concept written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-23 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: A proposed wing-body reusable launch vehicle was tested in the NASA Marshall Space Flight Center's 14 x 14-inch trisonic wind tunnel during the winter of 1994. This test resulted in the vehicle's subsonic and transonic, Mach 0.3 to 1.96, longitudinal and lateral aerodynamic characteristics. The effects of control surface deflections on the basic vehicle's aerodynamics, including a body flap, elevons, ailerons, and tip fins, are presented. Springer, A. M. Marshall Space Flight Center AERODYNAMIC CHARACTERISTICS; AERODYNAMIC FORCES; AERODYNAMIC STABILITY; ANGLE OF ATTACK; BODY-WING CONFIGURATIONS; CONTROL SURFACES; LATERAL STABILITY; LONGITUDINAL STABILITY; MACH NUMBER; SIDESLIP; SINGLE STAGE TO ORBIT VEHICLES; SPACECRAFT STABILITY; SUBSONIC SPEED; TRANSONIC SPEED; WIND TUNNEL TESTS; AILERONS; ELEVONS; FINS; PITCHING MOMENTS; ROLLING MOMENTS; YAWING MOMENTS...

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

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 Computational Study of a McDonnell Douglas Single Stage To Orbit Vehicle Concept for Aerodynamic Analysis

Download or read book Computational Study of a McDonnell Douglas Single Stage To Orbit Vehicle Concept for Aerodynamic Analysis written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of a computational flow analysis of the McDonnell Douglas single-stage-to-orbit vehicle concept designated as the 24U. This study was made to determine the aerodynamic characteristics of the vehicle with and without body flaps over an angle of attack range of 20-40 deg. Computations were made at a flight Mach number of 20 at 200,000 ft. altitude with equilibrium air, and a Mach number of 6 with CF4 gas. The software package FELISA (Finite Element Langley imperial College Sawansea Ames) was used for all the computations. The FELISA software consists of unstructured surface and volume grid generators, and inviscid flow solvers with (1) perfect gas option for subsonic, transonic, and low supersonic speeds, and (2) perfect gas, equilibrium air, and CF4 options for hypersonic speeds. The hypersonic flow solvers with equilibrium air and CF4 options were used in the present studies. Results are compared with other computational results and hypersonic CF4 tunnel test data. Prabhu, Ramadas K. Langley Research Center NAS1-19000; RTOP 242-20-80-02...