Download or read book Dual chamber Controllable Solid Propellant Rocket Motor Volume i Research and Development Efforts written by NORTHROP CAROLINA INC ASHEVILLE NC. and published by . This book was released on 1965 with total page 485 pages. Available in PDF, EPUB and Kindle. Book excerpt: The development of propellants for the forward and aft grains was completed by means of laboratory evaluations and subscale motor tests. Present technology was demonstrated by testing full-scale motors containing 300 lb of propellant both at sea-level and altitude. Excellent results were achieved in these tests in which the motors were programmed for both pulse and throttling operation. Thrust ratios as high as 9 to 1 were achieved. Another full-scale test series was conducted to demonstrate the technology advancements made throughout the entire three-year effort. These motors contained the advanced propellants developed during the program, an improved control valve and control system, and nozzles specifically designed for on-off motor operations. Tests of these 300-lb motors were conducted both at sea level and altitude. One of these motors demonstrated nine stop-restart cycles at altitude conditions. A full- scale test that fully demonstrated the feasibility of adapting the DCCSR concept to a post-boost propulsion system was also conducted.

Download or read book DUAL CHAMBER CONTROLLABLE SOLID PROPELLANT ROCKET MOTOR VOLUME 2 ANALYTICAL STUDY written by and published by . This book was released on 1965 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt: Trends and optimum conditions of mass fraction, boost-velocity, and motor envelope with variations in motor performance parameters and propellant characteristics for the dual-chamber controllable solid propellant rocket motor concept were studied. Five independent variables (motor performance parameters and propellant characteristics were selected for this study: (1) total impulse, (2) minimum thrust, (3) thrust throttling range, (4) number of on-off cycles available, and (5) motor specific impulse. The first four variables define the capability of a throttleable stop-restart motor, and each directly affects mass fraction, boost velocity, and motor envelope. The fifth variable, which is a function of propellant composition, directly affects motor size and boost velocity.

Download or read book Solid Propellant Rocket Research written by Martin Summerfield and published by Elsevier. This book was released on 2013-11-11 with total page 713 pages. Available in PDF, EPUB and Kindle. Book excerpt: Solid Propellant Rocket Research

Download or read book Solid Rocket Propulsion Technology written by A. Davenas and published by Newnes. This book was released on 2012-12-02 with total page 623 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book, a translation of the French title Technologie des Propergols Solides, offers otherwise unavailable information on the subject of solid propellants and their use in rocket propulsion. The fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following chapters. Specific design methods and the theoretical physics underlying them are presented, and finally the industrial production of the propellant itself is explained. The material used in the book has been collected from different countries, as the development of this field has occurred separately due to the classified nature of the subject. Thus the reader not only has an overall picture of solid rocket propulsion technology but a comprehensive view of its different developmental permutations worldwide.

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 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 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 Analytical and Experimental Studies of Spherical Solid propellant Rocket Motors written by Joseph G. Thibodaux and published by . This book was released on 1957 with total page 44 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 Innovative Energetic Materials Properties Combustion Performance and Application written by WeiQiang Pang and published by Springer Nature. This book was released on 2020-07-04 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book focuses on the combustion performance and application of innovative energetic materials for solid and hybrid space rocket propulsion. It provides a comprehensive overview of advanced technologies in the field of innovative energetic materials and combustion performance, introduces methods of modeling and diagnosing the aggregation/agglomeration of active energetic metal materials in solid propellants, and investigates the potential applications of innovative energetic materials in solid and hybrid propulsion. In addition, it also provides step-by-step solutions for sample problems to help readers gain a good understanding of combustion performance and potential applications of innovative energetic materials in space propulsion. This book serves as an excellent resource for researchers and engineers in the field of propellants, explosives, and pyrotechnics.

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 Solid Propellant Rocket Research written by Martin Summerfield and published by . This book was released on 1960 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Development and Evaluation of Solid Propellant Rocket Motor Case Insulating Materials Systems written by James D. Batchelor and published by . This book was released on 1960 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Notices of Changes in Classification Distribution and Availability written by and published by . This book was released on 1987 with total page 428 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid Propellant Rockets written by Clayton Huggett and published by . This book was released on 2016-04-19 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Download or read book Solid Propellant Rocket Research written by Martin Summerfield and published by . This book was released on 1960 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: