Session
Technical Session VI: Secondary Launch Opportunities
Abstract
Small satellite programs are often faced with the prospect of flying as a secondary payload because of size or funding considerations. This paper discusses a concept for flying such payloads on flights already scheduled on the Titan SLV program over the next decade. The Titan II has the capability of inserting over 4200 Ibs into Low Earth Orbit (LEO) and larger payloads on ballistic trajectories from which higher orbits can be achieved when kick motors are used. Orbit changes are possible depending on the specific altitudes and payloads involved. Of the existing 13 remaining missions currently scheduled to fly on the Titan II SLV, excess performance is available on several missions that could be used to insert secondary payloads of up to 3000 Ibs into their final orbit. This paper outlines an approach that would implement a secondary payload mission and allow small satellites to schedule a launch at a predetermined date through the year 2000.
Titan II Secondary Payload Capability
Small satellite programs are often faced with the prospect of flying as a secondary payload because of size or funding considerations. This paper discusses a concept for flying such payloads on flights already scheduled on the Titan SLV program over the next decade. The Titan II has the capability of inserting over 4200 Ibs into Low Earth Orbit (LEO) and larger payloads on ballistic trajectories from which higher orbits can be achieved when kick motors are used. Orbit changes are possible depending on the specific altitudes and payloads involved. Of the existing 13 remaining missions currently scheduled to fly on the Titan II SLV, excess performance is available on several missions that could be used to insert secondary payloads of up to 3000 Ibs into their final orbit. This paper outlines an approach that would implement a secondary payload mission and allow small satellites to schedule a launch at a predetermined date through the year 2000.
