Rocket power plants based on nitric acid and their specific propulsive weights / by Helmut Zborowski.

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Bibliographic Details
Main Author: Zborowski, Helmut
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Commitee for Aeronautics, [1947]
Series:Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 1145.
Subjects:

MARC

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245 1 0 |a Rocket power plants based on nitric acid and their specific propulsive weights /  |c by Helmut Zborowski. 
260 |a Washington, D.C. :  |b National Advisory Commitee for Aeronautics,  |c [1947] 
300 |a 22 pages, 16 unnumbered pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a Technical memorandums ;  |v no. 1145. 
500 |a "May 1947." 
500 |a NACA TM Number 1145. 
500 |a Translated from R-Antriebe, Schriften der Deutsche Akademie der Luftfahrtforschung, Number 1071, Nr. 82, pp. 91-126, by the National Advisory Commitee for Aeronautics. 
520 3 |a Two fields are reserved for the application of rocket power plants. 
520 3 |a The first field is determined by the fact that the rocket power plant is the only type of power plant that can produce thrust without dependence upon environment. For this field, the rocket is therefore the only possible power plant and the limit of what may be done is determined by the status of the technical development of these power plants at the given moment. 
520 3 |a The second field is that in which the rocket power plant proves itself the most suitable as a high-power drive in free competition with other types of power plants. The exposition will be devoted to the demarcation of this field and its division among the various types of rocket power plants. 
650 0 |a Rocket engines.  |0 http://id.loc.gov/authorities/subjects/sh85114703. 
650 0 |a Rockets (Aeronautics)  |x Fuel.  |0 http://id.loc.gov/authorities/subjects/sh85114725. 
650 0 |a Propellants.  |0 http://id.loc.gov/authorities/subjects/sh85107485. 
650 0 |a Rocket engines  |x Thrust.  |0 http://id.loc.gov/authorities/subjects/sh85114709. 
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650 7 |a Rocket engines  |x Thrust.  |2 fast  |0 (OCoLC)fst01099315. 
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830 0 |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ;  |v no. 1145.  |0 http://id.loc.gov/authorities/names/no2009014150. 
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