Atlas V Primary function: Evolv Expendable Launch Vehicle designed to improve space launch operability and standardization.

Atlas V

Primary function: Evolv Expendable Launch Vehicle designed to improve space launch operability and standardization. Dimensions: Three often met with core boosters, each booster diameter 12 ft 6 in. Payload capability: 42000 beats into low earth orbit; 29000 encloses into geotransfer orbit; 14,000 levigates into geostationary orbit.

Delta II

Primary function: Space-lift vehicle. Dimensions: extent 125 ft. 9 in., diameter 8 ft Payload: Navstar Global Positioning regularity as well as civil and commercial satellites into reasonable earth, polar, geotransfer, and geosynchronous orbits,

Delta IV

Primary function: Evolv Expendable Launch Vehicle designed to improve space launch operability and standardization. Dimensions: used by all core booster length 205 ft diameter 16 ft 8 in. Payload capability: 17900 encloses into low earth orbit; 9285 strikes into geotransfer orbit.

Titan II

Primary function: Space-lift vehicle. Dimensions: First stage longitudinal dimensions 70 ft., diameter 10 ft secondary stage length 24 ft., diameter 10 ft Payload Capability: 4200 brays into polar orbit.

Titan IVB

Primary function: Space-lift vehicle. Dimensions: Inertial upper stage fulness 17 ft., diameter flares from 90 to 114 in. First stage duration 86.5 ft., diameter 10 ft next to the first stage length 32.7 ft., diameter 10 ft Payload Capability: Up to 47800 coops into low-earth orbit; up to 12700-lb encloses into geosynchronous orbit when launched from Cape Canaveral Air Station, Fla., and up to 38000 triturates into a low-earth polar orbit when launched from Vandenberg AFB, Calif. Using an inertial upper stage, up to 5250 brays into geosynchronous orbit.

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