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Apollo Lunar Module J-mission configuration

The J-mission Lunar Module configuration supported the extended Apollo 15, 16, and 17 surface expeditions. Compared with the earlier H-mission lander, it carried more consumables and descent propellant, longer-stay thermal provisions, expanded scientific payload capacity, and the Lunar Roving Vehicle. LM-10 Falcon, LM-11 Orion, and LM-12 Challenger all landed successfully.

Apollo Lunar Module J-mission configuration
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Identity

Aliases
J-mission Lunar Moduleextended-stay Apollo LMApollo J-class LM
Family Name
Apollo Lunar Module
Full Name
Apollo Lunar Module J-mission configuration
Roles
crewed_spacecraftlander
Status
retired
Type
spacecraft
Variant Name
J-mission configuration

Details

Description
The J-mission Lunar Module configuration supported the extended Apollo 15, 16, and 17 surface expeditions. Compared with the earlier H-mission lander, it carried more consumables and descent propellant, longer-stay thermal provisions, expanded scientific payload capacity, and the Lunar Roving Vehicle. LM-10 Falcon, LM-11 Orion, and LM-12 Challenger all landed successfully.
First Flight Year
1,971
Last Flight Year
1,972
Manufacturer
Operator
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Nested value
    • Nested value
    Name
    Apollo Lunar Module J-mission propulsion
    Notes
    The Apollo 15–17 J-mission Lunar Module configuration used one descent propulsion system for powered lunar descent and one ascent propulsion system for lunar-surface liftoff and rendezvous.
Spacecraft Specs
Reusability
expendable

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Assets & Meta

Creation Time
July 14, 2026 at 18:51:03 UTC
Updated Time
August 1, 2026 at 08:20:48 UTC

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Search Name
Apollo Lunar Module J-mission configuration J-mission Lunar Module extended-stay Apollo LM Apollo J-class LM