SRM-30 rocket motor
- Thrust: 340 Newtons
- Burn time: 0.755 seconds
- Operating pressure: 62 bar
- Thrust profile: neutral (within 9-10%)
- Manufacturing materials: Al casing, steel nozzle/bulkhead
- Ignition: electric, 2 Amps at 12 Volts
- FLIGHT TESTED
N.B. The performance relates to a low-cost propellant, of Isp ~ 150 seconds. We can easily substitute this for higher-performance propellants, for extended thrust duration.
The 31 mm motor under test
The motor can be manufactured in different lengths, for burn times other than described above.
A performance certificate issued by ELMEC, Ploiesti, Romania, is available.