This paper describes the development and testing of a microthrust stand in the Advanced Propulsion Technology Laboratory at NASA/JPL.
Performance measurements using a sub-micronewton resolution thrust stand
International Elective Propulsion Conference
2001-10-15
Conference paper
No indication
English
Design and Performance Study of a Micronewton Thrust Stand for FEEP
British Library Online Contents | 1997
|Design and Performance Study of a Micronewton Thrust Stand for FEEP
British Library Conference Proceedings | 1997
|