Effective Specific Impulse of a Pulsed Rocket Engine
Description:
The specific impulse achieved in a pulsed rocket engine augmented with a fissioning nuclear bomb could be greater than that of any continuous flow engine. To a certain extent, this increase in specific impulse would be obtained at the expense of motor weight and average thrust. This paper considers the first of these limitations, motor weight, and estimates the highest effective specific impulse to be expected from a nuclear-pulsed rocket motor with respect to the weight of the motor.
Date:
May 5, 1965
Creator:
Platt, E. A. & Hanner, D. W.
Item Type:
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Partner:
UNT Libraries Government Documents Department