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Galileo Jupiter Orbiter propulsion module

NASA's Galileo spacecraft propulsion module was an integrated hypergolic system with twelve 10 N thrusters and one 400 N engine. It used monomethylhydrazine fuel and nitrogen tetroxide oxidizer; the thrusters and main engine supported spacecraft attitude, trajectory, and orbital maneuvers. NASA identifies Messerschmitt-Bolkow-Blohm as the developer and builder and the Federal Republic of Germany as provider. This record represents the complete installed orbiter propulsion module and does not create separate component identities.

Identity

Aliases
Galileo propulsion moduleGalileo retro-propulsion moduleGalileo orbiter propulsion
Domains
spaceflight
Identity Level
integrated-system
Kind
integrated-propulsion-system
Name
Galileo Jupiter Orbiter propulsion module
Status
retired

Details

Description
NASA's Galileo spacecraft propulsion module was an integrated hypergolic system with twelve 10 N thrusters and one 400 N engine. It used monomethylhydrazine fuel and nitrogen tetroxide oxidizer; the thrusters and main engine supported spacecraft attitude, trajectory, and orbital maneuvers. NASA identifies Messerschmitt-Bolkow-Blohm as the developer and builder and the Federal Republic of Germany as provider. This record represents the complete installed orbiter propulsion module and does not create separate component identities.
Propellants
monomethylhydrazinenitrogen tetroxide

Links

Assets & Meta

Creation Time
September 7, 2026 at 22:00:26 UTC
Updated Time
September 7, 2026 at 22:00:26 UTC

Other

Search Name
Galileo Jupiter Orbiter propulsion module Galileo propulsion module Galileo retro-propulsion module Galileo orbiter propulsion
Sources
  • Accessed Date
    2026-09-07
    Note
    NASA identifies Galileo's propulsion module as twelve 10 N thrusters and one 400 N engine using monomethylhydrazine fuel and nitrogen tetroxide oxidizer, and identifies MBB development/build with German provision.
    Publisher
    NASA Science
    Title
    Galileo
  • Accessed Date
    2026-09-07
    Note
    NASA's factsheet repeats the twelve 10 N and single 400 N propulsion-module architecture and the monomethylhydrazine/nitrogen-tetroxide propellant pair.
    Publisher
    NASA
    Title
    Galileo Mission to Jupiter
  • Accessed Date
    2026-09-07
    Note
    NASA technical-report metadata identifies the Galileo Retro-Propulsion Module and its in-flight characterization context.
    Publisher
    NASA Technical Reports Server
    Title
    Final Galileo Propulsion System In-Flight Characterization