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Author: John E. Dalgleish Publisher: ISBN: Category : Aeronautics Languages : en Pages : 20
Book Description
Experiments have been conducted with a jacketed rocket combustion chamber that was fabricated by hydraulic forming from sheet metal. Rocket combustion chambers made by this method have been used successfully. Runs with these combustion chambers have been made at over-all heat-transfer rates of 2.5 Btu per square inch per second with water cooling and also the ammonia as a regenerative coolant.
Author: John E. Dalgleish Publisher: ISBN: Category : Aeronautics Languages : en Pages : 20
Book Description
Experiments have been conducted with a jacketed rocket combustion chamber that was fabricated by hydraulic forming from sheet metal. Rocket combustion chambers made by this method have been used successfully. Runs with these combustion chambers have been made at over-all heat-transfer rates of 2.5 Btu per square inch per second with water cooling and also the ammonia as a regenerative coolant.
Author: John E. Dalgleish Publisher: ISBN: Category : Rockets (Aeronautics) Languages : en Pages : 11
Book Description
Experiments have been conducted with a jacketed rocket combustion chamber that was fabricated by hydraulic forming from sheet metal. Rocket combustion chambers made by this method have been used successfully. Runs with these combustion chambers have been made at over-all heat-transfer rates of 2.5 Btu per square inch per second with water cooling and also the ammonia as a regenerative coolant.
Author: Publisher: ISBN: Category : Languages : en Pages : 55
Book Description
An experimental investigation was conducted to determine the feasibility and practicality of the dual rocket motor concept. Cold flow studies were performed with the aid of a ground-test simulator which incorporated a telescoping booster cavity. The effects of booster cavity length, booster cavity shockdown pressure, booster/sustainer nozzle area ratios, and aft nozzle removal on thrust and performance were explored and discussed. (Author).
Author: James Francis McFillin (Jr) Publisher: ISBN: Category : Aeronautics Languages : en Pages : 48
Book Description
An experimental investigation was conducted to determine the feasibility and practicality of the dual chamber rocket concept. Cold flow studies were performed which utilized a telescoping booster cavity. The effects of booster cavity length, booster cavity shockdown pressure, booster/sustainer nozzle area ratio, and aft nozzle removal on thrust and the booster cavity pressure distribution were explored. (Author).
Author: James W. Wiggins Publisher: ISBN: Category : Airplanes Languages : en Pages : 692
Book Description
An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral stability of a complete-model swept-wing configuration at high subsonic speeds. The results indicate that, in a general, Mach number effects within the range studied and wing effects on the tail contribution were small and the overall trends of the data of the present investigation agreed with those which have been established at low speeds.
Author: John E. Dalgleish
Author: John E. Dalgleish
Author: John E. Dalgleish
Author: 
Author: Leonard V. Clark
Author: James Francis McFillin (Jr)
Author: United States. National Advisory Committee for Aeronautics
Author: James G. Lucas
Author: Army Library (U.S.)
Author: James W. Wiggins
Author: John L. Sloop