Systems:

• Vacuum Arc Thruster
• Vacuum Arc Ion Thruster
• Field Emission Electric Propulsion Thruster
• Low-mass PPU Systems for Low Power Operation
  

Applications

• Small satellite propulsion
• Fine positioning of larger systems and/or satellite constellations
  

Characteristics

• “Throttleability”
• Precise, small impulse bits
• Low overall thruster mass
• High efficiency
• High thrust/system mass ratio
  

Business relationships

• Aerojet General (strategic partner)
• USAF, NASA (customer)
• UIUC, MTU (AASC supplies propulsion systems)