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Spacecraft propulsion / Spacecraft design / Astronautics / Spacecraft / Attitude control / Reaction wheel / Pulsed plasma thruster / Capacitor / Spaceflight / Aerospace engineering / Space technology


Pulsed Plasma Thruster (PPT) Validation Report June 23, 2002 Chuck Zakrzwski NASA Goddard Space Flight Center
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Document Date: 2004-10-01 11:09:05

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File Size: 1,55 MB

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City

MATLAB / Beltsville / Greenbelt / performed using a high-fidelity MATLAB-based simulation to evaluate the EO-1 attitude control performance / /

Company

Attitude Control Electronics / PPT / General Dynamics / Primex Aerospace Corporation / EMC / Hammers Company / /

Event

Business Partnership / /

Facility

Capacitor Voltage Main Capacitor Temperature PPT Transformer Temperature Fuel Bar / Scott Benson NASA Glenn Research Center / Fuel Bar / /

IndustryTerm

minimum energy / fluid-propellant propulsion systems / control software cycle / electric propulsion devices / limited mechanical mounting hardware / propulsion technology / electronics / on-board control algorithm / imaging / technology validation / energy / /

Organization

PPT Command / National Aeronautics and Space Administration / NASA Goddard Space Flight Center / PPT GSE / EO-1 mission / Scott Benson NASA Glenn Research Center Cleveland / Inertial Reference Unit / /

Person

Chuck Zakrzwski / /

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Position

PID controller / controller / /

ProvinceOrState

Ohio / Virginia / Maryland / /

Technology

on-board control algorithm / broadband / 2.1 TECHNOLOGY / simulation / EO-1 technologies / propulsion technology / /

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