Journal
JOURNAL OF PROPULSION AND POWER
Volume 33, Issue 4, Pages 830-841Publisher
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.B36120
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- Eagleworks team
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A vacuum test campaign evaluating the impulsive thrust performance of a tapered radio-frequency test article excited in the transverse magnitude 212 mode at 1937MHz has been completed. The test campaign consisted of a forward thrust phase and reverse thrust phase at less than 8x10-6torr vacuum with power scans at 40, 60, and 80W. The test campaign included a null thrust test effort to identify any mundane sources of impulsive thrust; however, none were identified. Thrust data from forward, reverse, and null suggested that the system was consistently performing with a thrust-to-power ratio of 1.2 +/- 0.1mN/kW.
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