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The Effect Of Combustion Gas Flow On The Rotational Dynamics Of A Spinning Solid Fuel Rocket
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Book Synopsis The Effect of Combustion Gas Flow on the Rotational Dynamics of a Spinning Solid Fuel Rocket by : Paul Alexander Finlayson
Download or read book The Effect of Combustion Gas Flow on the Rotational Dynamics of a Spinning Solid Fuel Rocket written by Paul Alexander Finlayson and published by . This book was released on 1987 with total page 214 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 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Evaluation of Tangential Velocity Effects on Spinning Transverse Combustion Instability by : Marcus F. Heidmann
Download or read book Evaluation of Tangential Velocity Effects on Spinning Transverse Combustion Instability written by Marcus F. Heidmann and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Solid Rocket Motor Performance Analysis and Prediction by : William H. Miller
Download or read book Solid Rocket Motor Performance Analysis and Prediction written by William H. Miller and published by . This book was released on 1971 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The General Motion of a Variable-mass Flexible Rocket with Internal Flow by : Leonard Meirovitch
Download or read book The General Motion of a Variable-mass Flexible Rocket with Internal Flow written by Leonard Meirovitch and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: Dynamic motion characteristics of variable-mass flexible rocket with internal flow.
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 1020 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1970 with total page 796 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 1416 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis American Doctoral Dissertations by :
Download or read book American Doctoral Dissertations written by and published by . This book was released on 1997 with total page 806 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Relations of Combustion Dead Time to Engine Variables for a 20,000-pound-thrust Gaseous-hydrogen by : Daniel I. Drain
Download or read book Relations of Combustion Dead Time to Engine Variables for a 20,000-pound-thrust Gaseous-hydrogen written by Daniel I. Drain and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experiments were conducted on an uncooled 20,000lb-thrust gaseous-H and LOX rocket engine over a range of chamber pressure from 45 to 300 psia and oxidant-fuel ratio from 2 to 7. Combustion dead times were measured and compared with dead times calculated from frequency data for two assumed combustion models. Measured combustion dead time decreased with increasing chamber pressure at constant oxidant-fuel ratio or LOX injection velocity. This dead time also decreased with oxidant-fuel ratio at constant chamber pressure or O injection velocity. For the engine model where combustion dead time was considered to be the inverse of twice the measured chamberpressure frequency, only a fair agreement with the measured dead time was obtained. When the measured chamber-pressure frequencies were corrected for gas-dynamics effects in terms of the gas residence time, close agreement with the measured dead times was obtained. (Author).
Book Synopsis Three-dimensional Acoustic-rotational Flows in Solid-fuel Rocket Motors by : Peter Lindsay Staab
Download or read book Three-dimensional Acoustic-rotational Flows in Solid-fuel Rocket Motors written by Peter Lindsay Staab and published by . This book was released on 1998 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis OAR Cumulative Index of Research Results by :
Download or read book OAR Cumulative Index of Research Results written by and published by . This book was released on with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis OAR Quarterly Index of Current Research Results by : United States. Air Force. Office of Aerospace Research
Download or read book OAR Quarterly Index of Current Research Results written by United States. Air Force. Office of Aerospace Research and published by . This book was released on 1965 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fluid Mechanics of Spinning Rockets by : G. A. Flandro
Download or read book Fluid Mechanics of Spinning Rockets written by G. A. Flandro and published by . This book was released on 1987 with total page 179 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of a detailed investigation of the influence of time-dependent combustion gas flows on the attitude dynamics of spinning rocket propelled space vehicles. The work was motivated by a need to understand the origins of a potentially serious system performance problem first detected in the PAM-D series of spin stabilized upper stages. Small wobbling (often referred to as nutation or coning) induced during separation of the rocket motor burn. The growth ceased abruptly at motor burnout, and final cone angles as large as 17 deg were reached in some flights. The same phenomenon was encountered in two flights of the PAM-DII, a similar vehicle utilizing a larger motor. Conventional theories of spinning rocket dynamics failed to explain this behavior. Since the telemetry data shows that the severity of the problem depends on spacecraft mass properties and other system parameters, it is crucial that the origins of the instability be understood completely in order that serious mission degradation can be avoided in future orbit raising operations. A costly interim fix, which sidesteps the need to understand the physical origins of the problem, is the use of a strap-on nutation control system as used in the Air Force SGS II missions. This approach is in direct conflict with the philosophy of solid rocket space propulsion, which is based on its inherent simplicity and low cost.
Book Synopsis Gas Dynamic Flow in a Spinning, Coning Solid Rocket Motor by : D. L. Misterek
Download or read book Gas Dynamic Flow in a Spinning, Coning Solid Rocket Motor written by D. L. Misterek and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index to American Doctoral Dissertations by :
Download or read book Index to American Doctoral Dissertations written by and published by . This book was released on 1989 with total page 1252 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Thermogasdynamics of Solid-fuel Rocket Engines by : Ruvim Evelevich Sorkin
Download or read book The Thermogasdynamics of Solid-fuel Rocket Engines written by Ruvim Evelevich Sorkin and published by . This book was released on 1968 with total page 362 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report is concerned with gas-dynamic and thermodynamic problems of the theory of solid-propellant rocket engines. The author discusses in consecutive order the following: information of external ballistics, gas dynamics and thermodynamics; theory of the Laval nozzle; methods of calculation of equilibrium composition of products of fuel combustion in the chamber and nozzle; thermodynamic design of a rocket engine; calculation of parameters of internal ballistics with variable burning surface and with chemically reacting products of fuel combustion both for parameters of combustion products averaged in the chamber volume and for the plan of one-dimensional motion in the chamber and nozzle; methods of solving equations of internal ballistics for the igniter period; combined charge and packet of engines. (Author).
