CLLARE Design/Launch vehicle
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This page is part of an implementation of the CSTART Engineering Process. Anyone can edit it, but it should only be modified in accordance with the procedures and guidelines of the Process. Please check before editing if you are in doubt.
This document is a leaf node in the Design Task Tree for the CLLARE project.
Contents |
[edit] Summary
The purpose of this design task is to select a commercial launch vehicle(s) for suborbital launches and orbital insertions of the various CLLARE hardware configurations.
[edit] Inter-relations
This design task is inter-related with the following other design tasks:
- CLLARE Design/Launch site (the suppliers of different launch vehicles offer different candidate launch sites)
[edit] Background
[edit] Features/Considerations
- Reliability
- Cost
[edit] Requirements
[edit] Available Solutions
[edit] SpaceX Falcon 1-e
Might be able to lift an OSM-CM to orbit?
[edit] SpaceX Falcon 9
Should be able to lift a PM-PSM-CM-LL to orbit.
