Titan 2 missle silo
The Titan II was an intercontinental ballistic missile(ICBM) and space launcher developed by the Glenn L. Martin Company from the earlier Titan I missile. Titan II was originally designed and used as an ICBM, but was later used as a medium-lift space launch vehicleto carry payloads for the United States Air Force(USAF), National Aeronautics and Space Administration (NASA) and National Oceanic and Atmospheric Administration (NOAA). Those payloads included the USAF Defense Meteorological Satellite Program (DMSP), the NOAA weather satellites, and NASA's Gemini manned space capsules. The modified Titan II SLVs (Space Launch Vehicles) were launched from Vandenberg Air Force Base, California up until 2003. Sorry I haven't posted in a while but that's because I was working on this. I couldn't incorporate all details into this because it would be so massive and my phone can barely handle this. Ag 1 is the exploration vehicle it is also camera 1. Ag 2 is stage 2 to the missle. Ag3 is the first stage to the missle. Ag 6 is the elevator activated by vtol but normal vtol is the launch door. This does include a control room missle and full interior enjoy!
Specifications
General Characteristics
- Created On Android
- Wingspan 48.7ft (14.9m)
- Length 90.2ft (27.5m)
- Height 71.8ft (21.9m)
- Empty Weight 45,189lbs (20,497kg)
- Loaded Weight 53,191lbs (24,127kg)
Performance
- Wing Loading 439,839.3lbs/ft2 (2,147,483.6kg/m2)
- Wing Area 0.0ft2 (0.0m2)
- Drag Points 186121
Parts
- Number of Parts 1138
- Control Surfaces 0
- Performance Cost 3,780
Can you please delete this second post since there is two.