J Class Rocket Motor

Cesaroni 836J210-16A

Name: Cesaroni Technology 836J210-16A Rocket Motor
Creator: Veenie Aerospace
License: https://creativecommons.org/licenses/by/4.0/

Cesaroni Technology

Classic

Ø 54mm

Total Impulse

836.0Ns

Burn Time

3.99s

Avg Thrust

210.0N

Max Thrust

335.0N

Thrust Profile (N)

3.99s Burn Window

Engineered by Cesaroni Technology, the 836J210-16A is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 836.0 Ns over a 3.99 second burn window.

With an average thrust of 210.0 N and a peak of 335.0 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Classic propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry

Diameter 54 mm

Length 236 mm

Hardware Pro54-2G

Delays (s) 6,7,8,9,10,11,12,13,14,15,16

Specific Impulse 215.2 s

Peak Thrust 335 N

Peak Time T+ 0.04s

T/W Ratio 25.42

Propellant Classic

Profile regressive

Type reload

Sparky No

Mass Budget

842g Total

Casing (Dry)

446.0g

53.0%

Propellant

396.0g

47.0%

Live Sizing

Flight Envelope

Body Diameter 38 mm

Motor Mount 29 mm

Dry Mass 500 g

Target Apogee 1000 m

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