Download or read book Solid Rocket Motor Igniters NASA Space Vehicle Design Criteria Chemical Propulsion written by and published by . This book was released on 1971 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid Rocket Motor Igniters written by Donald H. Barrett and published by . This book was released on 1971 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid Propellant Rockets written by Clayton Huggett and published by Princeton University Press. This book was released on 2015-12-08 with total page 175 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 Ignition Systems Ii a Research Program for the Scientific Design of Igniters written by CHARLES F. SHARN and published by . This book was released on 1961 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: A practical program for the design of solid-rocket igniters is developed from an evaluation of rocket-ignition processes. The evaluation consists of: the derivation of igniion fundamentals from an analysis of combustion-ignition theory; the determination of rocket-ignition principles from an analysis of the important processes involved; and the development of anANALYTICAL, ROCKET-IGNITION MODEL TO DESCRIBE THE FUNCTION OF THE IGNITER IN THE IGNITION PROCESS. Based on the rocket-ignition model an engineering-type research program is constructed for the study of ignition in four basic phases: (1) the ignition system, (2) ignitability, (3) hydrodynamic phenomena, and (4) rocket ignition. The plan is to develop quantitative and qualittive ignier-design criteria through experimental and theoretical studies of each phase and the interrelations among the phases. (Author).

Download or read book Solid Rocket Propellants written by Haridwar Singh and published by Royal Society of Chemistry. This book was released on 2019-03-07 with total page 183 pages. Available in PDF, EPUB and Kindle. Book excerpt: Propellants contain considerable chemical energy that can be used in rocket propulsion. Bringing together information on both the theoretical and practical aspects of solid rocket propellants for the first time, this book will find a unique place on the readers' shelf providing the overall picture of solid rocket propulsion technology. Aimed at students, engineers and researchers in the area, the authors have applied their wealth of knowledge regarding formulation, processing and evaluation to provide an up to date and clear text on the subject.

Download or read book The Ignition of Cast Double Base Solid Propellant Rocket Motors by Pyrotechnic Igniters written by A. H. Trapp and published by . This book was released on 1975 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Measurement of Heat Flux from Igniters in Solid Propellant Rocket Motors written by K.M. Siddiqui and published by . This book was released on 1975 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of Atlas Solid Fuel Retarding Rocket During Atlas centaur Separation Tests written by and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: During the course of the Atlas Centaur separation tests in the Lewis Space Power Chamber recurrent failures were experienced in the firings of the Atlas retarding rockets. In an effort to evaluate the suitability of these rockets for flight use, an investigation into the primary cause for the misfires was instituted and an evaluation of the performance of the rockets was made. The primary cause of the failures of the rocket to ignite was inconsistent igniter functioning and a too short igniter burning period.

Download or read book Pyrogen Igniters for Solid Propellant Rocket Motors written by G. Sykes and published by . This book was released on 1981 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid propellant Rocket Ignition Systems Iv Evaluation of the Nol hi lo rocket in rocket Igniter written by CHARLES F. SHARN and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Measurement of Igniter Heat Flux in Solid Propellant Rocket Motors written by I. E. Smith and published by . This book was released on 1976 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Development of Wireless Ignition System WISys for Solid Rocket Motor written by Elexanderio Julit Anak Iling and published by . This book was released on 2013 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wireless igniter system (namely WISys in this research) is a modern type igniter system, which utilizes the concept of radio frequency (RF) communication between a transmitting device and a receiving device and also the usage of a specified designated igniter. This type of igniter system is now becoming the main focus in most rocketry industries, especially for small scale solid rocket motor (SRM). The main purpose of using a wireless igniter system is because it can provide secure feeling when conducting experiment and testing, especially when it comes to the matter of explosive materials. The main components that a wireless igniter system must have include a transmitter, a receiver and an igniter. In this research, both the transmitter and receiver were designed to be function able at various ranges and the maximum communication range must reach up to 100 meters. Therefore, selection for wireless communication module is very significant and here the XBee-S1 Starter Kit from Cytron Technologies was used as the main wireless communication module. With its ability to communicate with another XBee-S1 Starter Kit as far as 100 meters range and simplicity of performing configuration and synchronisation, the XBee-S1 Starter Kit module is simply the best choice, especially for those who are unfamiliar with radio frequency communication. Moreover, the power supply for the ignition must be at least 12V so that there is sufficient heating energy to ignite the pyrolant contained inside the igniter within 3 to 5 seconds. For a good igniter, the igniter must possess good characteristics, such as made from stainless steel, sustainable material, high melting point, able to withstand very high pressure and temperature, high resistance to rust, small size and portable, light weight and tough. So, igniter with these characteristics will be able to store enough pressure inside the combustion or primary chamber to achieve complete combustion of the pyrolant before it is forced out from the igniter into the thrust chamber of rocket motor to burn the propellant grains. As a conclusion, with high pressure inside the primary chamber the velocity inside the chamber would be low. Hence, the burning rate of the pyrolant would also be slower. With this condition achieved, the pyrolant inside the igniter could be burnt completely.

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 80 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 Ignition written by John Drury Clark and published by Rutgers University Press. This book was released on 2018-05-23 with total page 217 pages. Available in PDF, EPUB and Kindle. Book excerpt: This newly reissued debut book in the Rutgers University Press Classics Imprint is the story of the search for a rocket propellant which could be trusted to take man into space. This search was a hazardous enterprise carried out by rival labs who worked against the known laws of nature, with no guarantee of success or safety. Acclaimed scientist and sci-fi author John Drury Clark writes with irreverent and eyewitness immediacy about the development of the explosive fuels strong enough to negate the relentless restraints of gravity. The resulting volume is as much a memoir as a work of history, sharing a behind-the-scenes view of an enterprise which eventually took men to the moon, missiles to the planets, and satellites to outer space. A classic work in the history of science, and described as “a good book on rocket stuff…that’s a really fun one” by SpaceX founder Elon Musk, readers will want to get their hands on this influential classic, available for the first time in decades.

Download or read book Instantaneous Heat Transfer Pressure and Surface Temperature Characteristics of Solid Propellant Rocket Igniters written by J. Nanigan and published by . This book was released on 1960 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid propellant Rocket Ignition Research written by C. F. Sharn and published by . This book was released on 1964 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical and experimental study was made of solid rocket ignition for the purpose of obtaining igniter design criteria. Heat-transfer, ballistic, and ignition data were obtained by firing a rocket-type igniter, venting noncondensable products at an unsteady rate, into a small rocket. Measurements were made of igniter and rocket pressures, grain surface temperatures, and ignition times. In the tests, the heat fluxes ranged from 19 to 48 cal/sq. cm.-sec and ignition times from .002 to .015 sec. It was found that the ignition test data were in fair agreement to those predicted from the von Elbe ignition theory. An igniter design method, developed from test data and the von Elbe theory, is described. (Author).