APEx: ASCENT Propulsion Experiment

Program Management Review

Aug 2025

Discussion of overall satellite design.

Preliminary Design Review

Nov 2025

Avionics and software testing, detailed design concepts ready.

Critical Design Review

Nov 2026

Subsystem analyses complete; verification in progress.

Flight Selection Review

Jan 2027

Subsystem prototypes presented, engineering model complete.

Launch

Q2 2029

Spacecraft prepared for launch if selected post-FSR.

Future Work

The APEx team is currently performing system architecture trade studies and component selection, moving toward a more complete overall design of the satellite.

Current challenges include:

  • Selecting a propellant flow meter and tank gauging system
  • Designing a power and control board for the PMPD thruster
  • Defining thermal operating environments and control methods

The thruster prototype is still undergoing geometry optimization and propellant feed system design.

Overall Mission CONOPS diagram
Figure: Overall Mission CONOPS