Turbopump Related R&D Programs
- Air Force USET
- TR108 LOX/JP10, 30K lpf
- TR107 LOX/RP, 250K lbf
- Rapid design of low-cost turbopumps
- LOX/LH2 pump conceptual design
- LOX/Methane pump design through PDR
- Integrated Modular Machine
- LOX/Methane
- Turbopump design through conceptual design review
- Thrust Augmented Nozzle (TAN) studies
- HC/LOX booster application
- Trade studies and preliminary scoping of required turbomachinery
- Air Force TPA Additive Manufacturing for Reduced Costs
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Proprietary turbopump development projects for most of the leading established and emerging aerospace companies