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 |
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 |
Thrust Duration: | 3.2620 s |
Total Impulse: | 2760.8899 Ns |
Total Weight: | 2615.8000 g |
Type: | Reloadable |
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Date | Flyer | Rocket | Altitude |
---|---|---|---|
2014-04-11 | Gary Tortora | Stinger 6 | 4,414 Feet |
2013-05-04 | Gary Tortora | Performance Rocketry GIZMO XL | 3,834 Feet |
2013-04-06 | Mike Caplinger | ExW | 8,100 Feet |
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