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Book Experimental Performance of Nozzles Having Area Ratios Up to 300 on JP 4 Fuel   Liquid oxygen Rocket Engine

Download or read book Experimental Performance of Nozzles Having Area Ratios Up to 300 on JP 4 Fuel Liquid oxygen Rocket Engine written by J. Calvin Lovell and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract:

Book Experimental Performance of Nozzles Having Area Ratios Up to 300 on Jp 4 Fuel   Liquid oxygen Rocket Engine

Download or read book Experimental Performance of Nozzles Having Area Ratios Up to 300 on Jp 4 Fuel Liquid oxygen Rocket Engine written by J. Calvin Lovell and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: 4000-POUND-THRUST ROCKET ENGINE AT A CHAMBER PRESSURE OF 600 PSIA. Conic nozzles with area ratios of 8 and 25 had vacuum thrust coefficients at peak specific impulse equal to the values for theoretical frozen expansion. For conic nozzles having area ratios of 50, 100, 200 and 300 the thrust coefficients were higher than those for frozen expansion and equal to approximately 95% of the equilibrium expansion values. The arearatio-200 bell-shaped nozzles, which were 58% as long as the area-ratio-200, 15 degree half-angle conic nozzle, had thrust coefficients of 1.96, compared with 2.04 for the conic. (Author).

Book NASA Technical Note

    Book Details:
  • Author :
  • Publisher :
  • Release : 1962
  • ISBN :
  • Pages : 358 pages

Download or read book NASA Technical Note written by and published by . This book was released on 1962 with total page 358 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Performance of a High area ratio Rocket Nozzle at High Combustion Chamber Pressure

Download or read book Experimental Performance of a High area ratio Rocket Nozzle at High Combustion Chamber Pressure written by Robert S. Jankovsky and published by . This book was released on 1996 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the thrust coefficient of a high-area-ratio rocket nozzle at combustion chamber pressures of 12.4 to 16.5 MPa (1800 to 2400 psia). A nozzle with a modified Rao contour and an expansion area ratio of 1025:1 was tested with hydrogen and oxygen at altitude conditions. The same nozzle, truncated to an area ratio of 440:1, was also tested. Values of thrust coefficient are presented along with characteristic exhaust velocity efficiencies, nozzle wall temperatures, and overall thruster specific impulse.

Book NASA Memorandum

Download or read book NASA Memorandum written by and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1961-07 with total page 1766 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book International Aerospace Abstracts

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1996 with total page 1012 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft  Volume 3   Propulsion Subsystems  Performance  Stability and Control  Propellers  and Flight Safety

Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft Volume 3 Propulsion Subsystems Performance Stability and Control Propellers and Flight Safety written by Clifford J. Moore and published by . This book was released on 1970 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Memorandum

    Book Details:
  • Author : United States. National Aeronautics and Space Administration
  • Publisher :
  • Release : 1959
  • ISBN :
  • Pages : 620 pages

Download or read book NASA Memorandum written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1980 with total page 1132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Contractor Report

    Book Details:
  • Author : United States. National Aeronautics and Space Administration
  • Publisher :
  • Release : 1970
  • ISBN :
  • Pages : 1008 pages

Download or read book NASA Contractor Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 1008 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Study of Effects of Geometric Variables on Performance of Conical Rocket   Engine Exhaust Nozzles

Download or read book Experimental Study of Effects of Geometric Variables on Performance of Conical Rocket Engine Exhaust Nozzles written by Harry E. Bloomer and published by . This book was released on 1961 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: