Download or read book Development of a Multiple use Solid Rocket Motor written by Min Bing and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Studies Related to the Development of a Multiple Start stop Solid Propellant Rocket Motor written by Roger Alan Paulson and published by . This book was released on 1965 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Development of Large Solid Propellant Boosters written by United States. Congress. House. Committee on Science and Astronautics and published by . This book was released on 1962 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Engineering of Solid Rocket Motors written by José A. F. F. Rocco and published by Cambridge Scholars Publishing. This book was released on 2023-05-17 with total page 505 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the last few years, the aerospace industry has grown exponentially for both military and civil applications. This book explores the systems engineering, production processes and performance issues which happen constantly during solid rockets operations and flight. It also discusses state of the art experiments and techniques, as well as many recent developments. The book will appeal to rocket scientists, students and lecturers, senior scientists and professors.
Download or read book Propellant Development for the Advanced Solid Rocket Motor written by L. C. Landers and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The History of Large Solid Rocket Motor Development in the United States written by Wilbur C. Andrepont and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Material Development and the Solid Rocket Motor written by W.E. Bachrach and published by . This book was released on 1987 with total page 6 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Solid Propellant Processing Factors in Rocket Motor Design written by Carlton L. Horine and published by . This book was released on 1971 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Solid Propellant Grain Structural Integrity Analysis written by James S. Noel and published by . This book was released on 1973 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Development of the Explorer Solid Rocket Motor written by F. L. Sola and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Solid Rocket Motors written by United States. General Accounting Office and published by . This book was released on 1988 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Analytical Development of a Slotted Grain Solid Rocket Motor written by Roy J. Hartfield and published by . This book was released on 2002 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Captive fired Testing of Solid Rocket Motors written by James W. Kordig and published by . This book was released on 1971 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Feasibility Demonstration of a Single chamber Controllable Solid Rocket Motor written by Charles T. Levinsky and published by . This book was released on 1968 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary design phase, a propellant development phase, a lightweight motor development phase, and a lightweight motor demonstration phase were conducted. In the preliminary design phase, a trade-off study was conducted to size the system and a preliminary lightweight motor design was prepared and analyzed. In the propellant development phase, a family of extinguishable propellants was investigated. In the subscale design and development phase, the basic material selections were test fired in a motor which was designed to simulate the full-scale CSRM. In the heavyweight motor development phase, a full-scale CSR motor was designed and fabricated, three units were processed, and four tests conducted. In the lightweight motor development phase, the propellant was changed and the nozzle design was modified, four tests were conducted. In the demonstration phase, four motors were tested at Arnold Engineering Development Center, Tullahoma, Tennessee.
Download or read book Parallel Solution adaptive Method for Predicting Solid Propellant Rocket Motor Core Flows written by Jai Singh Sachdev and published by . This book was released on 2007 with total page 312 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computational framework has been developed for predicting two-dimensional axisymmetric turbulent multi-phase (gas-particle) solid propellant rocket motor core flows. The cornerstone of this numerical scheme is a parallel block-based adaptive mesh refinement (AMR) algorithm. AMR methods are effective in resolving the multiple solution scales typical of such complex fluid flow while minimizing computational expense. The use of body-fitted mesh blocks makes the application of the block-based AMR more amenable to flows with thin boundary layers and permits anisotropic refinement as dictated by initial mesh stretching. The block-based data structure lends itself naturally to domain decomposition and thereby enables efficient and scalable implementations of the algorithm on distributed-memory multi-processor architectures. A mesh adjustment scheme has been devised in which the body-fitted multi-block mesh is locally adjusted to arbitrarily embedded boundaries that are not necessarily aligned with the mesh. Not only does this scheme allow for rapid and robust mesh generation involving complex embedded boundaries, it also enables the solution of unsteady flow problems involving bodies and interfaces moving relative to the flow domain. This allows for the modelling and treatment of the pressure dependent burning of the solid propellant. The level set method is used to treat the evolution of the burning propellant surface. A Godunov-type finite-volume scheme has been developed to accurately predict the interaction between the gas and solid particles injected into the rocket chamber at the combustion interface. Standard fourth-order Runge-Kutta and second-order predictor-corrector time-marching schemes are used for time-accurate temporal discretization. An explicit optimally-smoothing multi-stage time-stepping scheme with multigrid convergence acceleration is used for obtaining steady state solutions. The mathematical characteristics of an Eulerian formulation for the particle-phase required the development of a new solution method for the particle-phase that allows for a more physically realistic solution than was previously attainable. A novel multi-velocity formulation is proposed that can account for crossing particle trajectories by splitting the particle-phase into distinct velocity families which are transported separately. The overall proposed methodology provides a state-of-the-art framework for accurately and efficiently predicting rocket motor core flows.
Download or read book Manuals Combined Early Solid Propellant Rocket Technology Studies written by and published by Jeffrey Frank Jones. This book was released on with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt: 1. Altitude Starting Tests of a 1000-Pound-Thrust Solid-Propellant Rocket Document ID: 20050019243 Author: Sloop, John L.; Rollbuhler, R. James; Krawczonek, Eugene M. Abstract: Four solid-propellant rocket engines of nominal 1000-pound-thrust were tested for starting hide Publication Year: 1957 Document Type: Technical Report Report/Patent Number: NACA-RM-E57G29 Date Acquired: Jan 11, 2005 2. Analytical and experimental studies of spherical solid-propellant rocket motors Document ID: 19930089785 Author: Thibodaux, Joseph G , Jr; Swain, Robert L; Wright, George Abstract: No Abstract Available Publication Year: 1957 Report/Patent Number: NACA-RM-L57G12a Date Acquired: Sep 01, 1996 3. Design and evaluation of a turbojet-exhaust simulator with a solid-propellant rocket motor for free-flight research Document ID: 19930089701 Author: Leiss, Abraham Abstract: No Abstract Available Publication Year: 1957 Report/Patent Number: NACA-RM-L57E10a Date Acquired: Sep 01, 1996 4. Flight Performance of a 2.8 KS 8100 Cajun Solid-propellant Rocket Motor Document ID: 19930089581 Author: Lee, Dorothy B Abstract: No Abstract Available Publication Year: 1957 Report/Patent Number: NACA-RM-L56K01 Date Acquired: Sep 01, 1996 5. Flight Investigation of the Performance of a Two-stage Solid-propellant Nike-deacon (DAN) Meteorological Sounding Rocket Document ID: 19930084525 Author: Heitkotter, Robert H Abstract: A flight investigation of two Nike-Deacon (DAN) two-stage solid-propellant rocket vehicles indicated hide Publication Year: 1956 Report/Patent Number: NACA-TN-3739 Date Acquired: Sep 01, 1996 6. The Design of a Miniature Solid-propellant Rocket Document ID: 19930084361 Author: Heitkotter, Robert H Abstract: No Abstract Available Publication Year: 1956 Report/Patent Number: NACA-TN-3620 Date Acquired: Sep 01, 1996 7. Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for use in Free-Flight Aerodynamic Research Models Document ID: 20050019463 Author: deMoraes, Carlos A.; Hagginbothom, William K., Jr.; Falanga, Ralph A. Abstract: A method has been developed for modifying a rocket motor so that its exhaust characteristics hide Publication Year: 1954 Document Type: Technical Report Report/Patent Number: NACA-RM-L54I15 Date Acquired: Jan 14, 2005 8. Some measurements of noise from three solid-fuel rocket engines Document ID: 19930084074 Author: Lassiter, Leslie W; Heikotter, Robert H Abstract: No Abstract Available Publication Year: 1954 Report/Patent Number: NACA-TN-3316 Date Acquired: Sep 01, 1996 9. Investigation of Vanes Immersed in the Jet of a Solid-fuel Rocket Motor Document ID: 19930087161 Author: Giladett, Leo V; Wineman, Andrew R Abstract: No Abstract Available Publication Year: 1952 Report/Patent Number: NACA-RM-L52F12 Date Acquired: Sep 01, 1996 10. An experimental investigation of the effect of high-pressure tailpipe length on the performance of solid-propellant motors for rocket-powered aircraft Document ID: 19930087092 Author: Rodriguez, Charles J Abstract: No Abstract Available Publication Year: 1952 Report/Patent Number: NACA-RM-L52E12a Date Acquired: Sep 01, 1996
Download or read book Solid rocket motor technology written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1979 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
