CTI 255H400-13A - Time-Thrust Curve and Data
The 255H400-13A (H400) is a 59% H 38mm 2-grain reloadable composite motor from Cesaroni Technology Incorporated (CTI).
This motor uses a Dipped E-Match igniter.
This reload fits a Pro38-2G motor case.
CTI's Vmax is a quick-burning propellant which produces a white flame and little smoke.
| Average Thrust: | 398.5594 N |
| Casing: | Pro38-2G |
| Class: | 59% H |
| Delays: | 4,6,8,10,14 s seconds |
| Designation: | 255H400-13A |
| Diameter: | 38.0000 mm |
| Formula: | Vmax |
| Igniter: | Dipped E-Match |
| Length: | 186.0000 mm |
| Letter: | H |
| Manufacturer: | CTI |
| Name: | H400 |
| Peak Thrust: | 439.1800 N |
| Propellant: | APCP |
| Thrust Duration: | 0.6400 s |
| Total Impulse: | 255.0780 Ns |
| Total Weight: | 283.6000 g |
| Type: | Reloadable |
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Flights
Date | Flyer | Rocket | Altitude |
|---|---|---|---|
2014-07-27 | Michael Freedman | Spitfire 2 | 2,071 Feet |
2014-01-11 | Jeffrey Gortatowsky | Nike-Smoke 2.6 | 3,274 Feet |
2012-08-19 | Tom Rankin | Cowabunga | - |
2010-04-24 | Howie Druckerman | Rebuild #2 | - |
2010-04-17 | Malcolm Smith | LOC/Precision Minie-Magg | - |
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