High power arcjet
THOMAS GOELZ, Monika Auweter‐Kurtz, Helmut Kurtz, H. O. Schrade
Abstract
THOMAS GOELZ, Monika Auweter‐Kurtz, Helmut Kurtz, H. O. Schrade
Abstract
The activities on the development of the high power arc jet HIPARC, the thrust balance, and plasma diagnostic probes are discussed. Modifications of the HIPARC design and a synopsis of the materials used are given. Further experimental results with the TT30 thruster in the 50 kW range are presented. Some first calibration measurements of the thrust balance are also included. Progress concerning the development of plasma diagnostic devices is documented.
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The activities on the development of the high power arc jet HIPARC, the thrust balance, and plasma diagnostic probes are discussed. Modifications of the HIPARC design and a synopsis of the materials used are given. Further experimental results with the TT30 thruster in the 50 kW range are presented. Some first calibration measurements of the thrust balance are also included. Progress concerning the development of plasma diagnostic devices is documented.
Key concepts: Arcjet rocket, Calibration, Thrust, Power (physics), Aerospace engineering, Plasma, Environmental science, Engineering