CTI 2856L910-P - Time-Thrust Curve and Data
The 2856L910-P (L910) is an 8% L 75mm 2-grain reloadable composite motor from Cesaroni Technology Incorporated (CTI).
This motor uses an E-Match igniter.
This reload fits a Pro75-2G 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: | 846.3795 N |
| Casing: | Pro75-2G |
| Certified By: | Canadian Association of Rocketry |
| Class: | 8% L |
| Delays: | Plugged |
| Designation: | 2856L910-P |
| Diameter: | 75.0000 mm |
| Formula: | C-Star |
| Igniter: | E-Match |
| Length: | 350.0000 mm |
| Letter: | L |
| Manufacturer: | CTI |
| Name: | L910 |
| Peak Thrust: | 1,047.5500 N |
| Propellant: | APCP |
| Status: | In-Production |
| Thrust Duration: | 3.2620 s |
| Total Impulse: | 2760.8899 Ns |
| Total Weight: | 2615.8000 g |
| Type: | Reloadable |
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