Measurement of the Maximum Altitude Attained by the X-15 Airplane Powered with Interim Rocket Engines
Author | : Wendell H. Stillwell |
Publisher | : |
Total Pages | : 16 |
Release | : 1960 |
Genre | : Rocket engines |
ISBN | : |
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Author | : Wendell H. Stillwell |
Publisher | : |
Total Pages | : 16 |
Release | : 1960 |
Genre | : Rocket engines |
ISBN | : |
Author | : Wendell H. Stillwell |
Publisher | : |
Total Pages | : 22 |
Release | : 1960 |
Genre | : Aerodynamics |
ISBN | : |
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 | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 448 |
Release | : 1960 |
Genre | : |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : |
Release | : 1960-07 |
Genre | : |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1300 |
Release | : 1978 |
Genre | : United States |
ISBN | : |