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Longitudinal And Lateral Directional Static Aerodynamic Characteristics Of An Unpowered Escape System Extraction Rocket Model With Attached Launch Tubes
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Book Synopsis Longitudinal and Lateral-directional Static Aerodynamic Characteristics of an Unpowered Escape System Extraction Rocket Model with Attached Launch Tubes by :
Download or read book Longitudinal and Lateral-directional Static Aerodynamic Characteristics of an Unpowered Escape System Extraction Rocket Model with Attached Launch Tubes written by and published by . This book was released on 1977 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal and Lateral-directional Static Aerodynamic Characteristics of an Unpowered Escape System Extraction Rocket Model by :
Download or read book Longitudinal and Lateral-directional Static Aerodynamic Characteristics of an Unpowered Escape System Extraction Rocket Model written by and published by . This book was released on 1977 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1977 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle (LEV) with Canard Surfaces Deployed by : William C. Moseley
Download or read book Aerodynamic Stability Characteristics of the Apollo Launch Escape Vehicle (LEV) with Canard Surfaces Deployed written by William C. Moseley and published by . This book was released on 1967 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Canted Forward Faces on the Static Longitudinal Stability Characteristics of the Escape and Exit Configurations of a Project Mercury Capsule Model at a Mach Number of 2.01 by : Roy V. Harris
Download or read book Effects of Canted Forward Faces on the Static Longitudinal Stability Characteristics of the Escape and Exit Configurations of a Project Mercury Capsule Model at a Mach Number of 2.01 written by Roy V. Harris and published by . This book was released on 1960 with total page 24 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 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 Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 by : Clarence A. Brown
Download or read book Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 written by Clarence A. Brown and published by . This book was released on 1962 with total page 86 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 Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration by : George M. Ware
Download or read book Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration written by George M. Ware and published by . This book was released on 1993 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges by : Joseph A. Yuska
Download or read book Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges written by Joseph A. Yuska and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal static stability characteristics of three one-fifth scale models of the second stage of a sounding rocket were calculated and compared with the measured values at Mach numbers of 1.79 to 3.47. All three models had fins of trapezoidal planform with sweptback leading and trailing edges, small aspect ratio, and thick wedge sections, but differed in fin area and overall model length. Calculation of center of pressure and normal-force coefficient slope at zero normal force were in good agreement with experimental data.
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1978 with total page 1266 pages. Available in PDF, EPUB and Kindle. Book excerpt: Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.
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 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 Longitudinal Aerodynamic Characteristics and Surface Pressure Measurements for a 1/10-scale Model of the RAM B Launch Vehicle by : Thomas C. Kelly
Download or read book Longitudinal Aerodynamic Characteristics and Surface Pressure Measurements for a 1/10-scale Model of the RAM B Launch Vehicle written by Thomas C. Kelly and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of an Ejection Seat Escape System with Cold Flow Rocket Plume Simulation at Mach Numbers from 0.6 Through 1.5 by :
Download or read book Aerodynamic Characteristics of an Ejection Seat Escape System with Cold Flow Rocket Plume Simulation at Mach Numbers from 0.6 Through 1.5 written by and published by . This book was released on 1969 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test was conducted in a transonic wind tunnel to determine the aerodynamic characteristics of a 0.5-scale ejection seat escape system with a dummy crew member attached during simulated rocket-off and rocket-on conditions. Results were obtained at free-stream Mach numbers of 0.6, 0.9, 1.2, and 1.5 through a model angle-of-attack range of 360 deg and model yaw angles up to 45 deg. High pressure air was used to simulate the escape rocket jet plume at altitudes from sea level to 40,000 ft. (Author).
