CTI 20146N5800-P - Time-Thrust Curve and Data

The 20146N5800-P (N5800) is a 99% N reloadable composite motor from Cesaroni Technology Incorporated (CTI).

This motor uses an E-Match igniter.

This reload fits a Pro98-6GXL 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: 5,667.1400 N
Casing: Pro98-6GXL
Class: 99% N
Delays: Plugged
Designation: 20146N5800-P
Diameter: 98.0000 mm
Formula: C-Star
Igniter: E-Match
Length: 1239.0000 mm
Letter: N
Manufacturer: CTI
Name: N5800
Peak Thrust: 6,957.2800 N
Propellant: APCP
Thrust Duration: 3.5900 s
Total Impulse: 20367.7000 Ns
Total Weight: 14826.0000 g
Type: Reloadable

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