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Massachusetts Institute of Technology

Simulation and design of a hydrogen arcjet thruster seeded with cesium

Abstract

dc:description.abstract

In conventional arcjets the largest loss in efficiency is the energy required to ionize the propellant. Adding a small amount of a readily ionizable material should provide adequate electrical conductivity, without the main propellant being ionized, thereby reducing this frozen loss. To study the effects of seeding a hydrogen arcjet with cesium, a two-dimensional numerical model was developed. The ions and atoms are treated as one fluid and the electrons as a second. The flow was modelled by Navier-Stokes equations modified to account for thermal and chemical non-equilibrium. The equations were numerically integrated by MacCormacks predictor-corrector scheme and a TVD scheme. The electric potential was solved by successive over-relaxation. Results show that the seeded arcjet can be run with the cesium fully ionized but the hydrogen having minimal dissociation or ionization. When the flow passes through the high current density region of the anode arc attachment, the hydrogen was found to not ionize as previously feared even when run at comparatively high currents. The cesium is fairly uniformly spread throughout the constrictor, as is the current density, so there is no formation of a narrow arc as in conventional thrusters.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2001

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Robertson, Darrel Kim, 1974-
Advisor dc:contributor.advisor
  • Manuel Martinez-Sanchez.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/8702
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/8702

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Robertson, Darrel Kim, 1974-. Simulation and design of a hydrogen arcjet thruster seeded with cesium. Massachusetts Institute of Technology, 2001. http://hdl.handle.net/1721.1/8702