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| | Conestoga - Space Launch System - United States (Site not responding. Last check: 2007-11-02) |
 | | Stage 1 uses two Thiokol Castor IVB motors that burn HTPB solid propellant, generating 96,037 lb of thrust each, and two Thiokol Castor IVA motors that burn HTPB solid propellant, generating 110,977 lb of thrust each |
 | | Stage 3 uses one Thiokol Castor IVB motor that burns HTPB solid propellant, generating 96,824 lb of thrust |
 | | Stage 4 uses one Thiokol Star 48V for injection that burns HTPB solid propellant, generating 15,355 lb of thrust (vacuum) |
| www.fas.org /spp/guide/usa/launch/conest.htm (183 words) |
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