Analysis Of Effects Of Rocket Engine Design Parameters On Regenerative Cooling Capabilities Of Several Propellants PDF Download
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Author | : Arthur N. Curren |
Publisher | : |
Total Pages | : 56 |
Release | : 1959 |
Genre | : Heat |
ISBN | : |
Download Analysis of Effects of Rocket-engine Design Parameters on Regenerative-cooling Capabilities of Several Propellants Book in PDF, ePub and Kindle
Author | : Dieter K. Huzel |
Publisher | : AIAA |
Total Pages | : 452 |
Release | : 1992 |
Genre | : Liquid propellant rocket engines |
ISBN | : 9781600864001 |
Download Modern Engineering for Design of Liquid-Propellant Rocket Engines Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 592 |
Release | : 1973 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : |
Release | : 1960-07 |
Genre | : |
ISBN | : |
Download Index to NASA Technical Publications Book in PDF, ePub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 448 |
Release | : 1960 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 494 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 296 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 860 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NACA Technical Publications Book in PDF, ePub and Kindle
Author | : William H. Robbins |
Publisher | : |
Total Pages | : 32 |
Release | : 1960 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download An Analysis of Nuclear-rocket Nozzle Cooling Book in PDF, ePub and Kindle
A nuclear-rocket regenerative-cooling analysis was conducted over a range of reactor power of 46 to 1600 megawatts and is summarized herein. Although the propellant (hydrogen) is characterized by a large heat-sink capacity, an analysis of the local heat-flux capability of the coolant at the nozzle throat indicated that, for conventional values of system pressure drop, the cooling capability was inadequate to maintain a selected wall temperature of 1440 R. Several techniques for improving the cooling capability were discussed, for example, high pressure drop, high wall temperature, refractory wall coatings, thin highly conductive walls, and film cooling. In any specific design a combination of methods will probably be utilized to achieve successful cooling.
Author | : |
Publisher | : |
Total Pages | : 1006 |
Release | : 1960 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews Book in PDF, ePub and Kindle