J Class Rocket Motor

SkyR J261G

Sky Ripper Systems
ABS/G, 830cc nitrous
Ø 54mm
Total Impulse
1248.0Ns
Burn Time
4.90s
Avg Thrust
262.0N
Max Thrust
2354.0N

Thrust Profile (N)

4.90s Burn Window

Engineered by Sky Ripper Systems, the J261G is a 54mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 1248.0 Ns over a 4.90 second burn window.

With an average thrust of 262.0 N and a peak of 2354.0 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration. It utilizes the ABS/G, 830cc nitrous propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 54 mm
Length 749 mm
Hardware 54/830
Delays (s) P
Specific Impulse 1398 s
Peak Thrust 1303.39 N
Peak Time T+ 0.02s
T/W Ratio 19.96
Propellant ABS/G, 830cc nitrous
Profile regressive
Type hybrid
Sparky No

Mass Budget

1338g Total
Casing (Dry)
1247.0g
93.2%
Propellant
91.0g
6.8%
Live Sizing
Flight Envelope

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