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 |
Class: | 51% I |
Delays: | 7,9,11,13,15,17 s seconds |
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 |
Thrust Duration: | 3.5000 s |
Total Impulse: | 484.7734 Ns |
Total Weight: | 594.0000 g |
Type: | Reloadable |
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