×
We have recently moved to a new server and are aware of issues with some images, the Rocksim library, and creating a new account. If you run into any other issues, please let us know through the Contact Us link at the bottom of the page. Thanks for visiting RocketReviews.
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 |
 |
 |
Blog Posts
Sponsored Ads
|
|