Search NASASearch

NASA NTRS · 19730009089

Thrust vectoring systems

Abstract

The design, fabrication, and testing of thrust vectorable ion optical systems capable of controlling the thrust direction from both 5- and 30-cm diameter ion thrusters is described. Both systems are capable of greater than 10 deg thrust deflection in any azimuthal direction. The 5-cm system is electrostatic and hence has a short response time and minimal power consumption. It has recently been tested for more than 7500 hours on an operational thruster. The 30-cm system is mechanical, has a response time of the order of 1 min, and consumes less than 0.3% of the total system input power at full deflection angle.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

King, H. J., Schnelker, D., Ward, J. W., Dulgeroff, C., Vahrenkamp, R.. 1972-12-01. Thrust vectoring systems. https://ntrs.nasa.gov/citations/19730009089

Cite the original work for its findings. Save a collection to share your selection of sources.