Measurement of the Maximum Altitude Attained by the X-15 Airplane Powered with Interim Rocket Engines PDF Download
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Author: Wendell H. Stillwell
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 16
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Book Description
Author: Wendell H. Stillwell
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 16
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Author: Wendell H. Stillwell
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
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Author: Wendell H. Stillwell
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
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Book Description
On August 4, 1960, a flight was made with the X-15 airplane to the maximum speed expected with the interim rocket engines. Fully corrected airspeed measurements showed that the maximum Mach number of 3/31 +/-0.04 and maximum true airspeed of 2,196 mph +/- 35 were attained at an altitude of 69,600 feet. At Mach numbers greater than 2.0 the pitot-static tube exhibited a negative static-pressure error which resulted in a Mach number correction of -0.18 at the maximum speed.
Author: Euclid C. Holleman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 30
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 478
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Author: United States. Superintendent of Documents
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Category : Government publications
Languages : en
Pages : 1812
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Author: United States. National Aeronautics and Space Administration
Publisher:
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Category : Aeronautics
Languages : en
Pages : 448
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450
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Author: United States. National Aeronautics and Space Administration
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Category :
Languages : en
Pages :
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Author:
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Category : Astrophysics
Languages : en
Pages : 724
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Covering the world's literature on meteorology, climatology, atmospheric chemistry and physics, physical oceanography, hydrology, glaciology, and related environmental sciences.
