CTI 518I165-17A - Time-Thrust Curve and Data
The 518I165-17A (I165) is a 51% I 54mm 1-grain reloadable composite motor from Cesaroni Technology Incorporated (CTI).
This motor uses an E-Match igniter.
This reload fits a Pro54-1G motor case.
CTI's C* propellant produces high performance and a bright flame. The propellant is identical to the formula used in the Space Shuttle's Solid Rocket Motor (SRM).
| Average Thrust: | 138.5067 N |
| Casing: | Pro54-1G |
| Certified By: | Canadian Association of Rocketry |
| Class: | 51% I |
| Delays: | 7,9,11,13,15,17 seconds (variable) |
| Designation: | 518I165-17A |
| Diameter: | 54.0000 mm |
| Formula: | C-Star |
| Igniter: | E-Match |
| Length: | 69.0000 mm |
| Letter: | I |
| Manufacturer: | CTI |
| Name: | I165 |
| Peak Thrust: | 188.6330 N |
| Propellant: | APCP |
| Status: | In-Production |
| Thrust Duration: | 3.5000 s |
| Total Impulse: | 484.7734 Ns |
| Total Weight: | 594.0000 g |
| Type: | Reloadable |
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