1–7 von 7 Ergebnissen
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    Qualification and life testing of a flight design hydrazine arcjet system

    KNOWLES, S. / YANO, S. / AADLAND, R. | AIAA | 1990

    Design for manufacturing improvements and demonstration of a 30 cm ion thruster

    King, D. / Meckel, N. / Aadland, R. et al. | AIAA | 2000

    Integrated mission simulation of a 26 kW flight arcjet propulsion system

    VAUGHAN, C. / CASSADY, R. / AADLAND, R. et al. | AIAA | 1993

    Development status of the BPT family of Hall Thruster systems

    Wilson, F. / King, D. / Willey, M. et al. | AIAA | 1999

    NEXT Ion Propulsion System Production Readiness AIAA Paper

    Hoskins, A. / Talerico, L. / Aadland, R. et al. | British Library Conference Proceedings | 2007

    A 26 KW Arcjet System for On-Orbit Demonstration

    Cassady, R. J. / Vaughan, C. E. / Aadland, R. S. et al. | British Library Conference Proceedings | 1992