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Titan 23G

Titan 23G was the orbital space-launch conversion of deactivated Titan II intercontinental ballistic missiles. Fourteen vehicles were selected for conversion, thirteen launched from Vandenberg Space Launch Complex 4 West between 1988 and 2003, and twelve of those launches succeeded.

Titan 23G
NASA/JPL · NASA/JPL asset; the exact PIA01480 page credits NASA/JPL. JPL current Image Use Policy permits images on public jpl.nasa.gov sites to be used for any purpose unless otherwise noted, with credit and without implying NASA, JPL, or Caltech endorsement. NASA/JPL logos and insignia, identifiable-person or privacy/publicity issues, and third-party materials noted in a caption remain separately restricted or clearance-sensitive; verify any commercial or promotional use. · Source
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Identity

Aliases
Titan II(23)GTitan 2(23)GTitan II SLVTitan 2GSB-4A
Family Name
Titan II
Full Name
Titan 23G
Status
retired
Type
rocket
Variant Name
23G

Details

Description
Titan 23G was the orbital space-launch conversion of deactivated Titan II intercontinental ballistic missiles. Fourteen vehicles were selected for conversion, thirteen launched from Vandenberg Space Launch Complex 4 West between 1988 and 2003, and twelve of those launches succeeded.
First Flight Year
1,988
Last Flight Year
2,003
Operator
Parent Vehicle Family
Rocket Specs
Reusability
expendable
Stages Count
2
Strap On Boosters Count
0

Links

Official Url
https://www.nasa.gov/wp-content/uploads/2023/04/sp-4012v7.pdf

Assets & Meta

Creation Time
July 17, 2026 at 06:22:55 UTC
Updated Time
July 19, 2026 at 10:05:44 UTC
Image
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Search Name
Titan 23G Titan II(23)G Titan 2(23)G Titan II SLV Titan 2G SB-4A