Ion Propulsion Technology Programs at NASA Glenn Research Center

التفاصيل البيبلوغرافية
العنوان: Ion Propulsion Technology Programs at NASA Glenn Research Center
المؤلفون: Patterson, M. J, Oleson, S. R
المصدر: Forum on Innovative Approaches to Outer Planetary Exploration 2001-2020.
بيانات النشر: United States: NASA Center for Aerospace Information (CASI), 2001.
سنة النشر: 2001
مصطلحات موضوعية: Lunar And Planetary Science And Exploration
الوصف: As lead center for the agency in electric and ion propulsion, the NASA Glenn Research Center (GRC) is pursuing technology development in ion propulsion for a range of mission applications. The program goal is to develop key technologies for advanced NSTAR-derivative high-power ion propulsion, lightweight low power high-performance ion propulsion, 'micro' ion propulsion, and engine and component technologies for high-power electric propulsion for very ambitious missions. Products include: (1) a 5 kW, 400 kg throughput ion thruster and power processing technology; (2) extremely-lightweight high-efficiency sub-kilowatt ion thruster and power processor; (3) a 1-25 W high-specific impulse ion engine; and (4) engine and component technologies for high-power (30 kW class) ion and Hall engines. Identified applications include outer planetary science missions such as Europa orbiter/lander, Comet Nucleus Sample Return mission, Titan Explorer, Neptune/Triton, Pluto-Kuiper Belt Objects Mission, various second generation interplanetary Micro spacecraft, and the Interstellar Probe Mission. Additional information is contained in the original extended abstract.
نوع الوثيقة: Report
اللغة: English
Relation: Forum on Innovative Approaches to Outer Planetary Exploration 2001-2020
URL الوصول: https://ntrs.nasa.gov/citations/20010041267
رقم الانضمام: edsnas.20010041267
قاعدة البيانات: NASA Technical Reports