Total Impulse
9.6Ns
Burn Time
0.96s
Avg Thrust
10.0N
Max Thrust
25.7N
Thrust Profile (N)
0.96s Burn WindowEngineered by Apogee Components, the C10 is a 18mm solid rocket motor designed for model rocketry. As an official C-class motor, it delivers a total impulse of 9.6 Ns over a 0.96 second burn window.
With an average thrust of 10.0 N and a peak of 25.7 N, it features a regressive thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.
Technical Specifications
National Association of RocketryDiameter 18 mm
Length 50 mm
Hardware Single Use
Delays (s) 4,7,10
Specific Impulse 198.9 s
Peak Thrust 25.72 N
Peak Time T+ 0.037s
T/W Ratio —
Propellant Standard
Profile regressive
Type SU
Sparky No
Mass Budget Unavailable
Live Sizing
Flight Envelope
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