Flight-proven pumps for propulsion and on-orbit fluid management:
- Designed for demanding space applications: propulsion, refueling, fluid transfer
- Wide range of sizes and fluids: green propellants (ASCENT, LMP-103S), hydrazine and hypergols (MMH, MON-3, MON-25), cryogenics (LN2, LOX, methane, propylene)
- Designed for launch and space environments (vibration, vacuum, radiation)
- Double seals (green propellants, inert fluids) or fully welded (hypergols)
- Customizable, option for customer configuration control
- Class 100 cleanliness for parts and assembly
- Full data packages available
- Full qualification and ATP testing available (vibration & thermal/thermal vacuum)
A complete family of pumps for most propulsion, refueling and fluid management applications:
| Application | Propulsion: 0.1 – 5 N Class | Propulsion: 20 N Monoprop 40 N Biprop | Propulsion: 45 N Monoprop 90 N Biprop | Propulsion: 100 N Monoprop 200 N Biprop | Propulsion: 450 N Monoprop 900 N Biprop | Fluid Cooling Systems | Cryogenic Fluid Transfer |
|---|---|---|---|---|---|---|---|
| Motor options | Brushless, Brushed | Brushless | |||||
| Typical Fluids | Hydrazine, MMH, NTO, MONs, Green Props | Water | LOX, LN2, LCH4 | ||||
| Performance* | 120.0 ml/min @ 350 psid | 500 ml/min @ 350 psid | 1.1 L/min @ 350 psid | 2.4 L/min @ 350 psid | 11.0 L/min @ 350 psid | 13 L/min @ 30 psid | 4.0 L/min @ 5 psid |
| Power class | 20 W | 50 W | 200 W | 400 W | 1.2 kW | 150 W | 90 W |
| Approx. Size | 22 mm x 100 mm | 22 mm x 120 mm | 30 mm x 145 mm | 43 mm x 300 mm | 60 mm x 400 mm | 110 mm x 180 mm | 42 mm x 120 mm |
| Approx. Mass | 230 g | 250 g | 900 g | 2 kg | 3.5 kg | 1.0 kg | 1.5 kg |
| TRL | TRL 9 for hydrazine & ASCENT TRL 8 for others | TRL 8 | TRL 8 | TRL 8 by Q4-25 | TRL 3 | TRL 8 | TRL 8 |
| Representative models & class (not to scale) |  22S |  22M |  30 |  40 |  60 |  30-W |  30-K |
* Representative performance listed; will vary with propellant and operating conditions