Measurement of Impulsive Thrust from a Closed Radio Frequency Cavity in Vacuum

التفاصيل البيبلوغرافية
العنوان: Measurement of Impulsive Thrust from a Closed Radio Frequency Cavity in Vacuum
المؤلفون: White, Harold, March, Paul, Lawrence, James, Vera, Jerry, Sylvester, Andre, Brady, David, Bailey, Paul
بيانات النشر: United States: NASA Center for Aerospace Information (CASI), 2016.
سنة النشر: 2016
مصطلحات موضوعية: Spacecraft Propulsion And Power
الوصف: A vacuum test campaign evaluating the impulsive thrust performance of a tapered RF test article excited in the TM212 mode at 1,937 megahertz (MHz) has been completed. The test campaign consisted of a forward thrust phase and reverse thrust phase at less than 8 x 10(exp -6) Torr vacuum with power scans at 40 watts, 60 watts, and 80 watts. 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 suggests that the system is consistently performing with a thrust to power ratio of 1.2 +/- 0.1 mN/kW.
نوع الوثيقة: Report
اللغة: English
URL الوصول: https://ntrs.nasa.gov/citations/20170000277
رقم الأكسشن: edsnas.20170000277
قاعدة البيانات: NASA Technical Reports