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Last Update: 11/19/02


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Validation Plan

Partners

PPO at NASA GRC

References


Credits
spacer image for layout NASA Official/Author: Nick Speciale

Curator:
Trish Johnson
Leslie Allen

Development Credits

Official Notice: Privacy Statement


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Pulsed Plasma Thruster title
spacer image for layout Summary    Overview     Benefits     Contacts
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The New Millennium Program's Earth Observing-1 mission (EO-1) provides for the first on-orbit demonstration of Pulsed Plasma Thruster photo a low mass, low cost, dependable electromagnetic Pulse Plasma Thruster (PPT) propulsion unit for precision attitude control.
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The PPT uses solid Teflon propellant and is capable of delivering high specific impulse (650-1400 sec), very fine impulse bits (90-1000µN-s) at low average power (12 to 70W). The PPT consists of a coiled spring to feed the Teflon propellant, an igniter plug to initiate a small trigger discharge and an energy storage capacitor and electrodes. Plasma is created by the ablation of the Teflon propellant from discharge of the storage capacitor across the electrodes. The plasma is accelerated by Lorenz force in the induced magnetic field to generate thrust.

The PPT is used to maintain fine pitch attitude control pointing requirements for EO-1 while meeting stringent electromagnetic and contamination constraints for the mission. A series of fine pitch pointing maneuvers have been conducted with the PPT activated after the EO-1 baseline mission was completed.

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section title : benefits
The PPT is applicable to Earth and space science missions requiring precision pointing and control. For example, the Origins Program will require precision alignment and coordination of multiple spacecraft. The PPT is a perfect candidate for these types of missions, and avoids liquid propellant sloshing which could effect instrument measurements.

Use of the PPT is particularly valuable in small spacecraft by offering a low mass and lower cost alternative to attitude control systems requiring reaction wheels and momentum unloading components. Also, the PPT may be an excellent low cost and low mass alternative for conventional delta-V propulsion systems. All of these benefits will help reduce the cost and weight of new Earth and space science missions.
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More Info Link Top of PageInstruments and Technologies page link
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section title: information contacts

Chuck Zakrwski
NASA's Goddard Space Flight Center
Mail Code: 574
Phone: (301) 286-3392
Email: Charles.M.Zakrzwski.1@gsfc.nasa.gov

Nick Speciale
EO-1 Mission Technologist
NASA's Goddard Space Flight Center
Mail Code: 490
Phone (301) 286-8704
Email: Nicholas.J.Speciale.1@gsfc.nasa.gov
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