Robust Scorpius®
Configuration Design -
- 3 stage-to-orbit allows use of high margin, moderate
performance components.
- Low-cost, all composite tanks.
- Low-cost ablative engines.
Simple Propulsion System -
- High performance Pressurization system.
- No turbopumps.
- No extendable or actively-cooled nozzles.
Multiple Similar Components -
- First and second stage employ (7) common pods.
- Larger quantity buys of smaller parts.
- 95% of vehicle weight is from common components
Low hardware costs allow Incremental Development -
- Scaleable system designs.
- Technologies demonstrated at small scale.
- Active (design, build, fly) team experience base.
Low-Complexity Production infrastructure -
- Flight-proven, low-cost valves.
- Smaller components and stages.
- In-house engine production.
- In-house tank production.
Efficient Operations Infrastructure -
- Launch within 8 hours of arrival of the payload at the launch
site.
- Air/Road transportable components.
- Single, non-toxic propellant type (Jet fuel and LOX).
Low-cost Component and Vehicle Level Testing -
- Avionics Lab.
- Cryogenic Flow Testing.
- TVC HWIL Testing.
- Vehicle Blowdown.
- Vehicle Hot-fire.
- Sub-orbital test.