CARWeb - Canadian Association of Rocketry / Association canadienne de fuséonautique Certified Motors | Level 1 Certification | Certified RSO List | Contact CAR/ACF
CAR/ACF Logo

 Regulations & Certifications 
 
HomeRegulationsInformationDocumentsLaunches

186-H42-10A Data

 
 
Motor Data
Brandname CTI 186-H42-MY-10A Manufacturer Cesaroni Technology
Man. Designation 186-H42-10A CAR/ACF Designation 186-H42-MY-10A
Test Date 2014-06-06
Single-Use/Reload/Hybrid Reloadable Motor Dimensions mm 29.00 x 231.00 mm (1.14 x 9.09 in)
Loaded Weight 242.00 g (8.47 oz) Total Impulse 186.00 Ns (41.85 lb/s)
Propellant Weight 105.50 g (3.69 oz) Maximum Thrust 83.50 N (18.79 lb)
Burnout Weight 125.00 g (4.38 oz) Avg Thrust 42.20 N (9.50 lb)
Delays Tested 10 - 1 s, adjustable ISP 179.31 s
Samples per second 1000 Burntime 4.41 s
Notes 16.2% H
 
Related
 
186-H42-10A Downloads
- Thrust Curve PDF
- RASP .eng File
- Certification Letter
 
Related Motors
 
CAR/ACF Motor Certification
 

Copyright 2024 - Canadian Association of Rocketry / Association canadienne de fuséonautique Email CAR/ACF President | Email WebAdmin | Contact CAR/ACF