CTI 5604M1830-P - Time-Thrust Curve and Data
The 5604M1830-P (M1830) is a 2% M 75mm 4-grain reloadable composite motor from Cesaroni Technology Incorporated (CTI).
This motor uses an E-Match igniter.
This reload fits a Pro75-4G 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: | 1,655.9870 N |
| Casing: | Pro75-4G |
| Certified By: | Canadian Association of Rocketry |
| Class: | 2% M |
| Delays: | Plugged |
| Designation: | 5604M1830-P |
| Diameter: | 75.0000 mm |
| Formula: | C-Star |
| Igniter: | E-Match |
| Length: | 621.0000 mm |
| Letter: | M |
| Manufacturer: | CTI |
| Name: | M1830 |
| Peak Thrust: | 2,300.7900 N |
| Propellant: | APCP |
| Status: | In-Production |
| Thrust Duration: | 3.1650 s |
| Total Impulse: | 5241.1988 Ns |
| Total Weight: | 4524.0000 g |
| Type: | Reloadable |
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