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An Investigation Of Base Heating On A 547 Per Cent Scale Model Of The Saturn S 1 Booster At Transonic Mach Numbers
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Book Synopsis An Investigation of Base Heating on a 5.47-per-cent Scale Model of the Saturn S-1 Booster at Transonic Mach Numbers by : T. L. Kennedy
Download or read book An Investigation of Base Heating on a 5.47-per-cent Scale Model of the Saturn S-1 Booster at Transonic Mach Numbers written by T. L. Kennedy and published by . This book was released on 1961 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the 16-ft transonic tunnel of the propulsion wind tunnel facility at the Arnold Center to evaluate base heating of the Saturn S-1 booster. Various turbine exhaust stack configurations were tested over a Mach number range of 0.6 to 1.5, an altitude range of 10,000 ft to 42,000 ft, and a missile angle-of-attack range of 0 to -7 1/2 deg. Rocket engines using liquid oxygen and RP-1 were used to simulate the full-scale engine exhaust, and hydrogen was used to simulate the turbo-pump exhaust. Base burning at all test conditions was eliminated for only one of the turbine exhaust stack configurations. Various degrees of base burning were obtained for all other exhaust stack configurations, but no burning occurred at a free-stream Mach number of 1.5 for the trajectory altitude. At altitudes above 29,000 ft, only localized base burning occurred and the accompanying heating rates were low.
Book Synopsis An Investigation of Base Heating on a 5.47-percent-scale Model Saturn Sa-1 Booster Afterbody at Mach Numbers 1.63 and 3.07 by : JOHN G. JR. DAWSON
Download or read book An Investigation of Base Heating on a 5.47-percent-scale Model Saturn Sa-1 Booster Afterbody at Mach Numbers 1.63 and 3.07 written by JOHN G. JR. DAWSON and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the base recirculation characteristics of several different turbine exhaust ducts on a 5.47% scale model of the Saturn SA-1 booster afterbody. Hydrogen gas was used to simulate the combustible products of the turbine exhaust. Base heating and base pressure data were taken with external airflow at Mach numbers 1.63 (33,000 to 45,000-ft altitude) and 3.07 (70,000 to 80,000ft altitude). The data indicated no base burning resulting from circulation of the combustible turbine exhaust gases. Flame shield calorimeter data indicated the maximum heat transfer rate at the center of the shield to be 113 Btu/sq ftsec. Flame shield pressure data indicated that the flow out from the flame shield region between adjacent engines became sonic at approximately 60,000-ft altitude. (Author).
Book Synopsis An Investigation of Base Heating with a 5.47-Percent Saturn SA-1 Booster Model at Mach Numbers 0.8 and 1.15 by : JOSEPH R. JR. PARKER
Download or read book An Investigation of Base Heating with a 5.47-Percent Saturn SA-1 Booster Model at Mach Numbers 0.8 and 1.15 written by JOSEPH R. JR. PARKER and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the base recirculation characteristics of the simulated propellant pump turbine exhaust gases of a 5.47-% scale model of the SA-1 Saturn afterbody. Gaseous hydrogen was used to simulate the combustible turbine exhaust gas of the fullscale missile. Base heating and pressure data were obtained at simulated flight trajectory conditions of M=0.8 0.8(16,000-ft) and M=1.15 1.15(27,500-ft) using several turbine exhaust duct configurations. In addition, the effect on base heating with one engine inoperative, of variation in turbine exhaust gas momen um, of finned-model operation, of variation in engine O/F ratio, and of variation in altitude was investigated. At both simulated flight trajectory conditions, the lowest base heating rates were obtained using a streamlined turbine exhaust duct configuration. The following conditions reduced base heating, based on data obtained with the long turbine exhaust ducts: operation with one engine inoperative, increased turbine exhaust gas discharge momentum, and increased engine O/F ratio. (Author).
Book Synopsis Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 by : Robert A. Wasko
Download or read book Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 written by Robert A. Wasko and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base-flow Aerodynamics of a Saturn-type Booster Stage at Mach Numbers 0.1 to 2.0 by : John L. Allen
Download or read book Base-flow Aerodynamics of a Saturn-type Booster Stage at Mach Numbers 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of the Base Environment of the Saturn S-IC Booster at Low Altitudes Using Short Duration Experimental Techniques by : E. A. Czeck
Download or read book An Investigation of the Base Environment of the Saturn S-IC Booster at Low Altitudes Using Short Duration Experimental Techniques written by E. A. Czeck and published by . This book was released on 1966 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Application of Short-duration Techniques to the Experimental Study of Base Heating by : K. C. Hendershot
Download or read book The Application of Short-duration Techniques to the Experimental Study of Base Heating written by K. C. Hendershot and published by . This book was released on 1965 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Lateral Vibration Characteristics of a 1/5-scale Model of Saturn SA-1 by : John S. Mixson
Download or read book Investigation of the Lateral Vibration Characteristics of a 1/5-scale Model of Saturn SA-1 written by John S. Mixson and published by . This book was released on 1961 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ by : Milton Lamb
Download or read book Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ written by Milton Lamb and published by . This book was released on 1976 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base Heat Transfer, Pressure Ratios and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Ratios and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base Heat Transfer, Pressure Rations and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at MAch Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Rations and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at MAch Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis PRESSURE TEST ON A 0.04-SCALE MODEL OF THE SATURN V LAUNCH VEHICLE AT MACH NUMBERS FROM 1.80 THROUGH 3.00 by :
Download or read book PRESSURE TEST ON A 0.04-SCALE MODEL OF THE SATURN V LAUNCH VEHICLE AT MACH NUMBERS FROM 1.80 THROUGH 3.00 written by and published by . This book was released on 1967 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: In conjunction with an earlier transonic test, a 0.04-scale model of the Saturn V launch vehicle was tested at Mach numbers from 1.80 to 3.00 for Reynolds number based on model diameter varying from 1.59 to 2.77 million. Static pressure distributions and boundary-layer profiles were measured and are presented herein.
Book Synopsis STATIC STABILITY AND PRESSURE TEST OF A 0.04-SCALE MODEL OF THE APOLLO SATURN V VEHICLE AT MACH NUMBERS FROM 0.60 THROUGH 1.40 by :
Download or read book STATIC STABILITY AND PRESSURE TEST OF A 0.04-SCALE MODEL OF THE APOLLO SATURN V VEHICLE AT MACH NUMBERS FROM 0.60 THROUGH 1.40 written by and published by . This book was released on 1968 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 0.04-scale model of the Saturn V Missile was tested at transonic Mach numbers to determine Reynolds number effects on static stability characteristics and pressure distributions in the tail barrel region at high angles of attack. Reynolds number based on the model diameter varied from 0.9 to 8.4 million. Angle of attack was varied from -3 to 16 deg. The center of pressure varied with angle of attack over a distance of approximately one model diameter.
Book Synopsis Flutter Test of an Array of Full-scale Panels from the Saturn S-ivb Stage at Transonic Mach Numbers by : T. M. Perkins
Download or read book Flutter Test of an Array of Full-scale Panels from the Saturn S-ivb Stage at Transonic Mach Numbers written by T. M. Perkins and published by . This book was released on 1968 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flutter characteristics of a 30-deg segment of the full-scale Saturn S-IVB stage were obtained at Mach numbers from 1.30 to 1.60 for various combinations of axial-compressive loads and panel differential pressures. Flutter was encountered in one or more panels when sufficient axial load was applied to either partially or completely buckle the panels. The flutter was amplitude limited, and no structural failures occurred on any of the panels as a result of flutter. However, the test had to be terminated when two panels in the fifth bay were statically buckled beyond their elastic limit and permanent deformation resulted. A calibration test was conducted prior to the flutter test to determine the optimum design of the fixture used to support the model. Also static-pressure and boundary-layer surveys were made on the model at tunnel conditions comparable to those of the flutter phase. (Author).
Book Synopsis Living and Working in Space by : William David Compton
Download or read book Living and Working in Space written by William David Compton and published by Courier Corporation. This book was released on 2013-05-13 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt: The official record of America's first space station, this book from the NASA History Series chronicles the Skylab program from its planning during the 1960s through its 1973 launch and 1979 conclusion. Definitive accounts examine the project's achievements as well as its use of discoveries and technology developed during the Apollo program. 1983 edition.
Book Synopsis Modern Engineering for Design of Liquid-Propellant Rocket Engines by : Dieter K. Huzel
Download or read book Modern Engineering for Design of Liquid-Propellant Rocket Engines written by Dieter K. Huzel and published by AIAA. This book was released on 1992 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
