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
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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