Titan II Launch Vehicle
The retired American two-stage Titan II launch vehicle, using twin LR87-AJ-5 first-stage engines and one LR91-AJ-5 second-stage engine.
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Identity
- Aliases
- Titan IISM-68BTitan 23G
- Family Name
- Titan II
- Full Name
- Titan II Launch Vehicle
- Roles
- -
- Status
- retired
- Type
- rocket
Details
- Description
- The retired American two-stage Titan II launch vehicle, using twin LR87-AJ-5 first-stage engines and one LR91-AJ-5 second-stage engine.
- First Flight Year
- 1,962
- Last Flight Year
- 1,987
- Propulsion Configurations
- Entries
- Count
- 2
- Placement
- core
- Propulsion System
- Role
- main
- Stage
- first-stage
- Variant Notes
- Twin Aerojet LR87-AJ-5 liquid-propellant engines.
- Count
- 1
- Placement
- upper
- Propulsion System
- Role
- upper-stage
- Stage
- second-stage
- Variant Notes
- Aerojet LR91-AJ-5 liquid-propellant engine.
- Name
- Titan II standard configuration
- Notes
- Titan II two-stage configuration with two LR87-AJ-5 engines on the first stage and one LR91-AJ-5 engine on the second stage.
- Rocket Specs
- Reusability
- expendable
- Stages Count
- 2
Links
- Wikipedia Url
- https://en.wikipedia.org/wiki/Titan_II
Assets & Meta
- Creation Time
- August 13, 2026 at 21:53:33 UTC
- Updated Time
- August 13, 2026 at 21:53:33 UTC