GH-N25
OVERVIEW
GH-N25 is our 25 Newton Green Hypergolic Vacuum Engine centered around a safer, cleaner, and equally performant green alternative to existing hypergolic bipropellant in-space propulsion systems.
We seek to address the longstanding drawbacks of hydrazine-based hypergolic bipropellant propulsion systems by developing and providing a propulsion architecture with the same ignition reliability, storability, and performance, without the toxicity.
DISPLAYED IS A RENDER OF THE GH-N25 RESEARCH ENGINE
TARGET PROPELLANT SPECIFICATIONS
SPECIFIC IMPULSE (VACUUM)
300s+
IGNITION DELAY
<10 ms (TARGET DELAY)
<20 ms (MAXIMUM ALLOWABLE DELAY)
TARGET PROPELLANT CHARACTERISTICS
Long-term Propellant Storability
Repeatable and Reliable Ignition
Reduced Toxicity with Improved Handling over Hydrazine-based Propellants
Suitability for both Main Propulsion and RCS Applications
get involved with GH-N25
Interested in GH-N25, our green hypergolic propellant, where it’s going, or want to get involved? Reach out to us today to see where the conversation takes us.