iPropulsion company research

DiscThruster

DiscThrusterTM is the pressure-thrust technology under development by iPropulsion.

Technical materials for pressure thrust, recirculation, and AIAA review.

Technology

DiscThruster applied to rocket engines and turbofan engines - Goals.

2X or doubling Specific impulse of modern rocket engine.
50% fuel flow reduction In thrust specific fuel consumption (TSFC) over modern turbofan engines.
DISRUPTOR Technology Including future endo/exoatmosphere commercial aircraft called AscentJet.

Papers

Author papers and supporting materials.

Published AIAA copies can be purchased through the linked AIAA paths where available.

DiscThruster Patent Application

US patent application documentation for the pressure-thrust aircraft engine concept.

Direct contact

Discuss iPropulsion research and DiscThruster materials.

Reach out for technical questions, document access, collaboration inquiries, or follow-up on the AIAA materials.