Total Impulse
648.5Ns
Burn Time
3.47s
Avg Thrust
270.0N
Max Thrust
427.6N
Thrust Profile (N)
3.47s Burn WindowEngineered by Ellis Mountain, the J270 is a 38mm solid rocket motor designed for high-power rocketry (HPR). As an official J-class motor, it delivers a total impulse of 648.5 Ns over a 3.47 second burn window.
With an average thrust of 270.0 N and a peak of 427.6 N, it features a regressive thrust curve optimal for general sport flying.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 38 mm
Length 384 mm
Hardware 38X438.1 38X467(D)
Delays (s) 20,P
Specific Impulse 190.5 s
Peak Thrust 386.52 N
Peak Time T+ 0.175s
T/W Ratio 38.66
Propellant Standard
Profile regressive
Type reload
Sparky No
Mass Budget
712g TotalCasing (Dry)
364.9g
51.2%
Propellant
347.1g
48.8%
Live Sizing
Flight Envelope
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Comparable J-Class Alternatives
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