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HiVHAc Hall propulsion system

NASA Glenn's HiVHAc is a 4 kW-class integrated Hall propulsion system combining a high-voltage Hall thruster, power-processing unit, and xenon flow-control module for lower-cost science and exploration missions.

Identity

Aliases
High Voltage Hall AcceleratorHiVHAc
Domains
spaceflight
Identity Level
integrated-system
Kind
integrated-propulsion-system
Name
HiVHAc Hall propulsion system
Status
development

Details

Description
NASA Glenn's HiVHAc is a 4 kW-class integrated Hall propulsion system combining a high-voltage Hall thruster, power-processing unit, and xenon flow-control module for lower-cost science and exploration missions.
Electric Specs
Input Power Kw Max
4
Propellants
xenon

Links

Assets & Meta

Creation Time
August 15, 2026 at 02:41:24 UTC
Updated Time
August 15, 2026 at 02:41:24 UTC

Other

Sources
  • Accessed Date
    2026-08-14
    Note
    NASA Glenn's paper defines HiVHAc as a 4 kW-class integrated propulsion system consisting of a Hall thruster, power-processing unit, and xenon flow-control module, with integrated closed-loop testing.
    Publisher
    NASA Technical Reports Server
    Title
    Performance of a High-Fidelity 4kW-Class Engineering Model PPU and Integration with HiVHAc System
  • Accessed Date
    2026-08-14
    Note
    NASA Glenn documents the HiVHAc development system, its 4 kW Hall-thruster class, and mission rationale for lower-cost electric propulsion.
    Publisher
    NASA Technical Reports Server
    Title
    Integration Tests of the 4 kW-class High Voltage Hall Accelerator Power Processing Unit with the HiVHAc and SPT-140 Hall Effect Thrusters