Rocket engine URM-1 is implemented on the rescue pilot seat type VS-1 BRI assigned for Czech aircraft L-39 Albatros. URM-1 is designed to accelerate pilot seat during its ejection. The purpose of this rocket engine is to raise pilot seat from the height level "Zero-Zero" on the height that enables safe parachute opening.
This TARA Aerospace AD Rocket Engine has been assigned with the NATO Codification System Number NSN 1377-77-000-0083.
Specifications
| Length | 410 mm |
| Diameter | 136 mm |
| Connections thread | M12 |
| Weight, approximate | 10 kg |
| Ignition with | two fuses UP-014 |
| Weight of the charge, approximate | 42 g |
| Weight of the propellant, approximate | 2.580 kg |
| Number of nozzles | 4 pcs. |
| Safe function in the temperature range | from -60°C to +60°C |
| Proper shipping name | Rocket motors |
| UN Number | 0280 |
| ADR Number | 1.1C |
| Packing Group | II |
Packing
2 rocket engines in one wooden box.
Dimensions 710 x 370 x 285 mm.
Shelf life
9 years from the date of manufacture in the store.
8 years on aircraft or 1600 flight hours.
