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Download e-book for iPad: Advanced Propulsion Systems and Technologies, Today to 2020 by Claudio Bruno, Visit Amazon's Antonio Accettura Page, search

By Claudio Bruno, Visit Amazon's Antonio Accettura Page, search results, Learn about Author Central, Antonio Accettura,

ISBN-10: 156347929X

ISBN-13: 9781563479298

"Commissioned through the ecu house business enterprise, this publication information particular propulsion applied sciences as anticipated via 2020. each one expertise has been thought of by way of suggestion, linked key applied sciences, improvement prestige and proposed roadmaps. The reader is led via the entire steps that propulsion will most probably take among now and the 2020s in a transparent, concise, and distinct approach, together with industry and feasibility views whilst applicable.
The sixteen chapters persist with a developmental common sense. the fabric starts off with the way forward for SRM, grounded on R&D performed at the moment, is going throughout the improvement of LOX/HC liquid rocket engines, a expertise in response to U.S. and Russian paintings of the 60s and 70s. It then seems to be into destiny applied sciences, and platforms simply commencing to make their effect felt now, resembling superconductivity utilized to electrical propulsion, MW-class ion engines (perhaps using a nuclear energy source), sunlight sails, laser propulsion, nuclear propulsion (such because the promising VASIMR), and ISRU."

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Extra info for Advanced Propulsion Systems and Technologies, Today to 2020

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AIAA, Reston, VA, 2004. 2 Rev. 1 P80 FW Motor, Avio - Colleferro (Rome), 2002. Bibliography Accettura, A. , “PROPULSION 2000 – Phase I Final Report,” NTEPRP 10000, Rome, Nov. 2000. 1. ,“Design and Development of Medium/Large Composite Cases for Solid Rocket Motors,” Second European Conference on Launcher Technology, Rome, 21–24 Nov. 2000. , “Industrial Constraints as Evaluation Criteria in Developing Solid Space Propellants Using Alternative Energetic Materials,” 36th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 1997–2975, July 1997.

S. shuttle; b) casting must be done in segments that must be assembled before launch; and c) casting must be carried on in a dedicated facility near the launch site. 4) Once ignited, they cannot be easily switched off; thereafter they need to be designed each for a specific mission. In this sense, they are the most inflexible among propulsion systems. The most important advantages of solid rocket boosters for commercial launchers are as follows: 1) high density and low volume; 2) very long, if not indefinite, storage life; 3) instant ignition without fueling operations; 4) high reliability; and 5) less expensive.

Improvements will either aim at an increase in reliability, an enhancement of performance, or a reduction of cost. A. Launcher Concept Currently there are two major types of space transportation systems operational: first, launchers with large strap-on boosters with core and upper stages (HII, SOYUZ and ARIANE) [2]; and second launchers with a booster, an optional sustainer, and an upper stage (ATLAS II and III, Delta II, PROTON K) [2, 3]. , 1000–2000 kN) but with a higher specific impulse and with operating times in the range of about 600 s.

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Advanced Propulsion Systems and Technologies, Today to 2020 by Claudio Bruno, Visit Amazon's Antonio Accettura Page, search results, Learn about Author Central, Antonio Accettura,

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