CTI 5472M2250-P - Time-Thrust Curve and Data
The 5472M2250-P (M2250) is a 7% 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: | 2,189.4200 N |
| Casing: | Pro75-4G |
| Class: | 7% M |
| Delays: | Plugged |
| Designation: | 5472M2250-P |
| Diameter: | 75.0000 mm |
| Formula: | C-Star |
| Igniter: | E-Match |
| Length: | 621.0000 mm |
| Letter: | M |
| Manufacturer: | CTI |
| Name: | M2250 |
| Peak Thrust: | 2,663.1700 N |
| Propellant: | APCP |
| Thrust Duration: | 2.5000 s |
| Total Impulse: | 5466.9800 Ns |
| Total Weight: | 4415.0000 g |
| Type: | Reloadable |
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Flights
Date | Flyer | Rocket | Altitude |
|---|---|---|---|
2016-06-10 | Mike Caplinger | ExW | 14,038 Feet |
2012-07-13 | Gary Tortora | Formula 150 | 8,346 Feet |
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