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Book Ramjet with Integrated Rocket Boost Motor

Download or read book Ramjet with Integrated Rocket Boost Motor written by John L. Leingang and published by . This book was released on 1972 with total page 5 pages. Available in PDF, EPUB and Kindle. Book excerpt: The patent application relates to a combination rocket motor ramjet engine having the rocket motor located in the ramjet inlet diffuser. All or part of the rocket portion of the apparatus remaining after rocket booster burnout are ejected by air pressure in the diffuser inlet to permit the diffuser to supply ram air for the ramjet engine.

Book A Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine Part 1  Transition from Rocket Booster to Ramject Sustainer

Download or read book A Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine Part 1 Transition from Rocket Booster to Ramject Sustainer written by Hong-Gye Sung and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Integral Hybrid boost solid fuel Ramjet Propulsion for Lightweight Tactical Missiles

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).

Book Integral Rocket Ramjet Demonstration Programme  IRRDP

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.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 426 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine

Download or read book Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine written by Hong-Gye Sung and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Ramjet Engines

    Book Details:
  • Author : Mikhail Makarovich Bondari͡u︡k
  • Publisher :
  • Release : 1969
  • ISBN :
  • Pages : 466 pages

Download or read book Ramjet Engines written by Mikhail Makarovich Bondari͡u︡k and published by . This book was released on 1969 with total page 466 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Official Gazette of the United States Patent and Trademark Office

Download or read book Official Gazette of the United States Patent and Trademark Office written by United States. Patent and Trademark Office and published by . This book was released on 1976 with total page 1164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Reverse Flow AFT Inlet Ramjet System

Download or read book Reverse Flow AFT Inlet Ramjet System written by Edward T. Curran and published by . This book was released on 1974 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The patent application concerns a combined rocket/ramjet for propelling a missile including a missile payload module and an integral rocket/ramjet engine system strapped on the missile payload module. It incorporates a liquid or solid fuel rocket engine and a ramjet engine having a combustion chamber common with the rocket engine, an exhaust nozzle, and multiple aft-mounted air inlets movable between a retracted position during rocket boost flight and an extended, pop-out position to receive and direct ram air in a reverse flow direction into the combustion chamber during ramjet flight.

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

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.

Book Theory of Ramjet and Rocket ramjet Engines

Download or read book Theory of Ramjet and Rocket ramjet Engines written by Vladimir Stepanovich Zuev and published by . This book was released on 1972 with total page 252 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Boron Based Fuel Rich Propellant

Download or read book Boron Based Fuel Rich Propellant written by WeiQiang Pang and published by CRC Press. This book was released on 2019-04-09 with total page 323 pages. Available in PDF, EPUB and Kindle. Book excerpt: Boron-Based Fuel-Rich Solid Rocket Propellant Technology is a professional book that systematically introduces the latest research progress for boron-based fuel-rich solid propellants. It covers surface modifications, coating and agglomerating techniques, granulation, and characterization of amorphous boron powders, and its application to fuel-rich solid rocket propellants. Technologies for controlling the processing methods and combustion performance of fuel-rich propellants are examined, and the book concludes with a summary of the research progress in boron-based fuel-rich solid propellants and a look forward to the foreseeable development trends of military applications.

Book Integral Rocket Ramjets

Download or read book Integral Rocket Ramjets written by R. F. Calzone and published by . This book was released on 1994 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt: A rough overview of the important aspects and problem areas associated with the development of Integral Rocket Ramjet (IRR) technology is given in this report. The IRR is a supersonic air-breathing concept in which the gas generator produces fuel-rich gases. These fuel-rich gases are burnt in the secondary combustion chamber with ambient air captured and decelerated in the inlet. During the boost phase, a solid propellant booster provides the thrust necessary to achieve the velocity at which the ramjet may be operated (about M = 2). The booster is integrated in the secondary combustion chamber.

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book AIAA ASME SAE ASEE 24th Joint Propulsion Conference

Download or read book AIAA ASME SAE ASEE 24th Joint Propulsion Conference written by and published by . This book was released on 1988 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Solid Rocket Propulsion Technology

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.