Accurate measurement of thrust from microthrusters is a significant technical challenge. We report significantly improved performance from our microthruster thrust stand which has now demonstrated 25nN thrust resolution and can carry a fully operational microthruster and power supply with up to 15kg total mass. Thrust capacity is 500μN with 0.5% accuracy and minimum response with 25% accuracy is 100nN. Because it is a critically‐damped torsion balance with tens‐of‐seconds response time, thrust readout noise is essentially absent for frequencies above 0.1 Hz. Other reported measurement techniques require careful leveling of the apparatus, or have higher readout noise, lower sensitivity and greater sensitivity to ambient mechanical vibrations. A key ingredient for the performance of our system design is an optical readout that responds only to rotation of the torsion bar, but not to ambient vibration. This feature eliminates sensitivity to footsteps, nearby vacuum pumps, etc. We will describe the design, calibration and testing of the optical readout.
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2 May 2006
BEAMED ENERGY PROPULSION: Fourth International Symposium on Beamed Energy Propulsion
15-18 November 2005
Nara (Japan)
Research Article|
May 02 2006
A Low‐Noise Thrust Stand for Microthrusters with 25nN Resolution Available to Purchase
Claude R. Phipps;
Claude R. Phipps
*Photonic Associates LLC, 200A Ojo de la Vaca Road, Santa Fe, New Mexico 87508
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James R. Luke;
James R. Luke
*Photonic Associates LLC, 200A Ojo de la Vaca Road, Santa Fe, New Mexico 87508
†NMT/IERA, 901 University Blvd. Albuquerque, NM, 87106
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Wesley Helgeson;
Wesley Helgeson
†NMT/IERA, 901 University Blvd. Albuquerque, NM, 87106
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Richard Johnson
Richard Johnson
†NMT/IERA, 901 University Blvd. Albuquerque, NM, 87106
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Claude R. Phipps
st
James R. Luke
st,gger
Wesley Helgeson
gger
Richard Johnson
gger
*Photonic Associates LLC, 200A Ojo de la Vaca Road, Santa Fe, New Mexico 87508
†NMT/IERA, 901 University Blvd. Albuquerque, NM, 87106
AIP Conf. Proc. 830, 492–499 (2006)
Citation
Claude R. Phipps, James R. Luke, Wesley Helgeson, Richard Johnson; A Low‐Noise Thrust Stand for Microthrusters with 25nN Resolution. AIP Conf. Proc. 2 May 2006; 830 (1): 492–499. https://doi.org/10.1063/1.2203291
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