Technical Resources
Engineering Data & Specs
Comprehensive technical documentation for integration engineers, propulsion teams, and safety officers.
Propellant Comparison
At a Glance
| Property | RP-1 | LOX | LH2 | UDMH | AF-M315E |
|---|---|---|---|---|---|
| State | Liquid | Cryogenic | Cryogenic | Liquid | Liquid |
| Density (g/cm³) | 0.81 | 1.14 | 0.071 | 0.79 | 1.47 |
| Boiling Point | 216°C | -183°C | -253°C | 63°C | N/A (ambient) |
| ISP (vacuum, s) | ~311 | Oxidizer | ~451 | ~285 | ~235 |
| Toxicity | Low | Non-toxic | Non-toxic | High | Low |
| Storage | Ambient | Cryo-tank | Cryo-tank | Sealed | Ambient |
| Our Purity | 99.998% | 99.999% | 99.9999% | 99.95% | 99.9% |
Documentation
Safety & Compliance Library
RP-1 Safety Data Sheet
Material safety, handling procedures, emergency response protocols.
Request AccessLOX Handling Manual
Cryogenic safety procedures, PPE requirements, storage guidelines.
Request AccessLH2 Technical Brief
Para-hydrogen conversion data, thermal management, venting procedures.
Request AccessGreen Propellant White Paper
Technical comparison of AF-M315E and LMP-103S vs. hydrazine.
Request Access
Certifications
Standards We Uphold
AS9100D
Aerospace QMS
ISO 9001:2015
Quality Management
ISO 14001
Environmental
ITAR
Export Controls
MIL-DTL-25576
RP-1 Specification
MIL-PRF-27201
LOX Specification
Need Detailed Technical Data?
Contact our engineering team for full specifications, COAs, and integration support documentation.