SMALL ROCKET LIFT DEVICE. PHASE 3. TESTING OF THE ASSEMBLED SYSTEM
Wendell F. Moore, J. Kroll, S. Borass, N. Carriero
Abstract
Wendell F. Moore, J. Kroll, S. Borass, N. Carriero
Abstract
The fabrication and testing of the Small Rocket Lift Device (SRLD) is reported. The effort consisted of 4 fundamental tasks: (1) The development of a suitable propellant quantity warning and indicating system; (2) The design and test of a paraglider lift augmentation device for use with the SRLD; (3) Performance of stability and control studies utilizing data in possession of the Contractor from an instrumented rocket belt flight test program to be conducted by the US Air Force; (4) Performance of a human factors study for the purpose of determining optimum trainee selection criteria and establishing SRLD training requirements.
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The fabrication and testing of the Small Rocket Lift Device (SRLD) is reported. The effort consisted of 4 fundamental tasks: (1) The development of a suitable propellant quantity warning and indicating system; (2) The design and test of a paraglider lift augmentation device for use with the SRLD; (3) Performance of stability and control studies utilizing data in possession of the Contractor from an instrumented rocket belt flight test program to be conducted by the US Air Force; (4) Performance of a human factors study for the purpose of determining optimum trainee selection criteria and establishing SRLD training requirements.
Key concepts: Lift (data mining), Propellant, Aeronautics, Rocket (weapon), Engineering, Aerospace engineering, Automotive engineering, Simulation