Download or read book Design and Testing of a Caseless Solid fuel Integral rocket Ramjet Engine for Use in Small Tactical Missiles written by Keith J. Fruge and published by . This book was released on 1991 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Integral Hybrid boost solid fuel Ramjet Propulsion for Lightweight Tactical Missiles written by Paul C. Woods and published by . This book was released on 1995 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the feasibility of a small, low-cost, caseless, hybrid-booster/solid-fuel ramjet (H/SFRJ) that utilizes a common fuel grain and has no ejectables. Performance of an air-to-ground missile with a solid propellant booster and SFRJ sustainer, capable of being fired from an unmanned aerial vehicle or helicopter was obtained using an Air Force computer code. A H/SFRJ motor was then designed analytically and compared to the generated computer output. The results showed that a H/SFRJ that has performance equal to a solid-booster SFRJ is feasible. The final missile design had a range of 20 nm, a flight Mach number of 2.0, a diameter and length of 5 and 99 inches respectively, and weighed 82 lb. Caseless hybrid rockets with erodible nozzles were tested to validate assumptions made in the design analysis. In addition, transition from hybrid-rocket booster to solid-fuel ramjet sustainer was demonstrated. (MM).
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Integral Rocket Ramjet Demonstration Programme IRRDP written by and published by . This book was released on 1998 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes the main accomplishments of a collaborative Canadian-Dutch project known as the Integral Rocket Ramjet Demonstration Program (IRRDP) to investigate the key technologies of air-breathing missile propulsion through the design, fabrication, & testing of a solid fuel ducted rocket engine with an integral booster for a medium-range air-launched missile. It begins by discussing the requirements for an integral rocket ramjet engine, then reviews activities related to the development of a missile design tool & performance prediction tool, computational fluid dynamics evaluation of the intake & port covers, development of a new solid propellant for a gas generator used in ducted rocket propulsion, modelling of the ramjet combustor in a water tunnel, combustion tests, modelling & propellant development for the nozzle-less booster, and the final design.
Download or read book Ramjet and Ramrocket Propulsion Systems for Missiles Held at Monterey California London United Kingdom and Neubiberg Germany F R on 5 6 10 11 and 13 14 September 1984 written by and published by . This book was released on 1984 with total page 241 pages. Available in PDF, EPUB and Kindle. Book excerpt: This lecture series provided an introduction to modern ramjet technology. Applications to missiles were especially emphasized. The survey and characterization of various types of ramjets were followed by the discussion of ramjet components. Three of the lectures dealt with the main types of subsonic combustion ramjets. One lecture was devoted to supersonic combustion ramjets. Titles include: Ramjet Air Induction System Design for Tactical Missile Application; Aspects of Engine and Airframe Integration for Ramjet and Ramrocket Powered Missiles; Integral Boost, Heat Protection, Port Covers and Transition; Special Problems of Ramjet with Solid Fuel; and Solid Propellant Ramrockets.
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 Government Reports Announcements Index written by and published by . This book was released on 1992-06 with total page 1516 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Annual Index written by and published by . This book was released on 1992 with total page 1400 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Study of test and evaluation on integral rocket ramjets for tactical missiles written by Hisahiro Nakayama and published by . This book was released on 2006 with total page 14 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 Subsonic Combustion Ramjet Design written by Antonella Ingenito and published by Springer Nature. This book was released on 2021-01-29 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book presents a step-by-step methodology for the design of ramjet engines. It explores ramjet combustion, provides guidelines on how to size the engines, and discusses performance analysis. The book begins with an introduction to ramjet design, including fundamental definitions in the field. It then discusses ramjet engine performance, and fuels which can be used. Several types of ramjet engines are then explored, and guidelines for their design are presented, including flame holders, injectors, and combustors. Finally, the book concludes with a discussion of the types of materials which should be used for ramjet engines. This book is of interest to engine designers and engineers, researchers, and graduate students, as it collates research in a succinct, clear guide to the issue of designing ramjet engines.
Download or read book A High performance 250 pound thrust Rocket Engine Utilizing Coaxial flow Injection of JP 4 Fuel and Liquid Oxygen written by Samuel Stein and published by . This book was released on 1959 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Studies of Solid Rocket Motor airframe Integration Design for Tactical Missile written by G. Y. Fang 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 Metallized Fuel Particle Size Study in a Solid Fuel Ramjet written by James Allen Nabity and published by . This book was released on 1989 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Particle size measurements were obtained at the grain exit and nozzle entrance in a solid fuel ramjet combustor using a boron based fuel. The particle size distributions at the aft end of the fuel grain were generally quadra-modal, with mode peaks at 2, 4,15, and 25 - 45 microns. At the nozzle entrance the distributions were tri-modal, due to the complete oxidation of the 2 micron particles. Sauter mean diameter and the size of the largest agglomerates increased with increasing equivalence ratio (or grain length), indicating that the longer grains result in more surface agglomeration. Combustion efficiency increased with equivalence ratio. A direct correlation of particle size alone with combustion efficiency was not obvious and may require an accurate measurement of particle concentration. Keywords: Integral rocket ramjet engines; Rocket propellant grains; Solid fuel ramjet engines; Combustion; Laser particle measurement; Metallized rocket fuels. Theses. (edc).
Download or read book Technology Test Bed written by and published by . This book was released on 1991 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Design Fabricate and Testing Small Rocket Motor written by Mohamad Izwan Ghazali and published by . This book was released on 2012 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt: There was a lot of study on Solid Rocket Motor (SRM) based solid propellant. This project focus on and discusses the study of optimum design based SRM characteristics including the methods of the optimum design selection and fabrication, analysis using COSMOS and static thrust testing. Before that, the researcher has focus on the fundamental of solid rocket motor for designing and fabricating. There are two main factors need to be considered in the design selection and fabrication which are performance or processability and mechanical strength. The theoretical performance of the propellant was obtained by using CHEM program. Together with literature study and theoretical performance, three models or design of nozzle with different size throat were finalized with consideration of the mechanical and processability factors. The propellant was a mixture of Potassium nitrate and sucrose. The rocket motors were manufactured or fabricated using lathe and milling machine. Then three solid rocket motors were tested to get the thrust and performance. The results show that the increasing of thrust and combustion pressure lead to the decreasing the throat size and increasing the throat length. The highest thrust was 1260N and burning time about 4 Sec. Meanwhile, for the performance characteristics, the specific impulse, Isp that obtained from static thrust testing for solid propellant was 4% lower than theoretically.
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:
