Showing papers on "Arcjet rocket published in 1969"
Patent•
24 Mar 1969TL;DR: In this article, a throttling mechanism for the nozzle of a solid-propellant rocket motor is proposed, which is capable of selectively controlling the effective area of the discharge orifices of the nozzle whereby the magnitude of the thrust of the rocket motor may be varied.
Abstract: A throttling mechanism for the nozzle of a solid propellant rocket motor that is capable of selectively controlling the effective area of the discharge orifices of the nozzle whereby the magnitude of the thrust of the solid propellant rocket motor may be varied.
9 citations
Patent•
01 Dec 1969
TL;DR: In this article, a system for controlling the operating pressure and thrust of a solid propellant rocket motor is described, which includes a propellant cutter that extends through the burning surface of the solid-pursuit to increase on command burning surface area and thereby increase the burning rate.
Abstract: A system for controlling the operating pressure and thrust of a solid propellant rocket motor which includes a propellant cutter that extends through the burning surface of the solid propellant to increase on command the burning surface area and thereby increase the burning rate of the solid propellant.
8 citations
TL;DR: In this article, the Doppler shift of spectral lines resulting from macroscopic velocities in axial and rotational directions was investigated with respect to the plasma jet, and it was shown that the shift is independent of the velocity of the jet.
Abstract: : The plasma jet was investigated with respect to the Doppler shift of spectral lines resulting from macroscopic velocities in axial and rotational directions. (Author)
6 citations
03 Mar 1969
1 citations