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| | Delta II Launch Vehicle |
 | | Delta II comprises a group of expendable rockets that can be configured as two- or three-stage vehicles and with three, four or nine strap-on graphite epoxy motors (GEMs) depending on mission needs. |
 | | Delta II payload delivery options range from about 891 to 2,142 kg (1,965 to 4,723 lb) to geosynchronous transfer orbit (GTO) and 2.7 to 6.0 metric tons (5,934 to 13,281 lb) to low-Earth orbit (LEO). |
 | | Two-stage Delta II rockets typically fly LEO missions, while three-stage Delta II vehicles generally deliver payloads to GTO or are used for deep-space explorations such as NASA's missions to Mars, a comet or near-Earth asteroids. |
| www.boeing.com /defense-space/space/delta/delta2/delta2.htm (315 words) |
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