1 N HPGP Thruster
ECAPS
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CU Aerospace offers comprehensive thrust measurement and verification for propulsion systems across a 500 µN to 500 mN range, accommodating test articles up to 20 kg. Utilizing a 0.8 m³ vacuum chamber, our facility supports both steady-state firing and impulsive bit testing across diverse pressure environments—from high-flow systems at 1 Torr to low-flow electric propulsion (EP) regimes reaching 1e-5 Torr.
Features:
- 500 µN – 500 mN range (may be expandable given application)
- High flow systems down to 1 Torr @ 200 mg/s
- Low flow, EP systems down to 1e-5 Torr
- Steady firing and impulsive bits
- 0.8 m3 vacuum chamber
- 20 kg maximum test article mass
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