Numerical Simulation of a Low-Power Hydrazine Arcjet Thruster
Author:
Publisher
Elsevier BV
Subject
General Engineering
Reference25 articles.
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2. G.W. Butler, R.J. Cassady (1996) Directions for Arcjet Technology Development. Journal of Propulsion and Power 12: 1026-1034.
3. M.A. Birkan (1996) Arcjets and Arc Heaters: An Overview of Research Status and Needs. Journal of Propulsion and Power 12: 1011-1017.
4. V.R. Watson, E.B. Pegot (1967) Numerical Calculations for the Characteristics of a Gas Flowing Axially Through a Constricted Arc. NASA Technical Note TN D-4042.
5. H.X. Wang, X. Chen, W.X. Pan, A.B. Murphy, J.Y. Geng, S.X. Jia (2010) Modelling Study to Compare the Flow and Heat Transfer Characteristics of Low-Power Hydrogen, Nitrogen and Argon Arc-Heated Thrusters. Plasma Science and Technology 12 (in press).
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3. Steady-state behavior of liquid fuel hydrazine decomposition in packed bed;AIChE Journal;2014-12-11
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