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Apollo 9 Gumdrop-Spider crewed lunar-module test spacecraft family

NASA Apollo 9 spacecraft family performed the first crewed flight of the complete Apollo configuration, testing the lunar module, rendezvous, docking, propulsion, navigation, and life-support systems in Earth orbit in March 1969.

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Identity

Aliases
Apollo 9Apollo 9 spacecraftGumdropSpiderApollo 9 command and service moduleApollo 9 lunar module
Family Name
Apollo 9
Full Name
Apollo 9 Gumdrop-Spider crewed lunar-module test spacecraft family
Roles
crewed_spacecraftorbiterlanderresearch
Status
retired
Type
spacecraft

Details

Description
NASA Apollo 9 spacecraft family performed the first crewed flight of the complete Apollo configuration, testing the lunar module, rendezvous, docking, propulsion, navigation, and life-support systems in Earth orbit in March 1969.
First Flight Year
1,969
Last Flight Year
1,969
Operator
Propulsion Configurations
  • Entries
    • Count
      1
      Placement
      spacecraft
      Propulsion System
      Role
      main
      Stage
      service-module
      Variant Notes
      Single Aerojet AJ10-137 Service Propulsion System on the Gumdrop service module; the existing Apollo CSM Block II integrated-system boundary is reused without changing the propulsion identity.
    • Count
      2
      Placement
      spacecraft
      Propulsion System
      Role
      attitude-control
      Stage
      command-module
      Variant Notes
      Two independent Command Module reaction-control subsystems; the existing Apollo CSM Block II installation establishes the subsystem count, not an inferred individual-engine model.
    • Count
      4
      Placement
      spacecraft
      Propulsion System
      Role
      attitude-control
      Stage
      service-module
      Variant Notes
      Four Service Module reaction-control quad packages distributed around the service-module periphery, matching the existing Apollo CSM Block II installation.
    Name
    Apollo 9 Gumdrop CSM Block II propulsion
    Notes
    Apollo 9 Gumdrop command-and-service-module propulsion only. The Block II boundary is represented by one AJ10-137 Service Propulsion System, two Command Module reaction-control subsystems, and four Service Module reaction-control quad packages. Saturn launch-vehicle propulsion and the separate Spider lunar-module systems remain outside this configuration.
  • Entries
    • Count
      1
      Placement
      spacecraft
      Propulsion System
      Role
      landing
      Stage
      descent
      Variant Notes
      One integrated Lunar Module Descent Propulsion System retained for the Apollo 9 LM test boundary; no mission-specific engine model is invented.
    • Count
      1
      Placement
      spacecraft
      Propulsion System
      Role
      takeoff-lift
      Stage
      ascent
      Variant Notes
      One integrated Lunar Module Ascent Propulsion System used for Apollo 9 ascent-stage firing and rendezvous operations; no exact engine variant is inferred from generic evidence.
    Name
    Apollo 9 Spider lunar-module propulsion
    Notes
    Apollo 9 Spider lunar-module main propulsion only. NASA documents the self-sufficient Lunar Module test and ascent-stage firing; the existing integrated Descent Propulsion System and Ascent Propulsion System identities are reused. The Lunar Module reaction-control system is intentionally omitted because no exact canonical LM-RCS dependency is present in this packet, and no new identity or engine model is inferred.

Assets & Meta

Creation Time
August 13, 2026 at 09:11:12 UTC
Updated Time
August 25, 2026 at 19:06:18 UTC
Apollo 9 Gumdrop-Spider crewed lunar-module test spacecraft family - AeroVia