Total Impulse
4995.4Ns
Burn Time
8.00s
Avg Thrust
600.0N
Max Thrust
1056.0N
Thrust Profile (N)
8.00s Burn WindowEngineered by Ellis Mountain, the L600 is a 76mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 4995.4 Ns over a 8.00 second burn window.
With an average thrust of 600.0 N and a peak of 1056.0 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts.
Technical Specifications
Tripoli Rocketry Association, Inc.Diameter 76 mm
Length 584 mm
Hardware Single Use
Delays (s) P
Specific Impulse 205.9 s
Peak Thrust 829.67 N
Peak Time T+ 0.186s
T/W Ratio 14.85
Propellant Standard
Profile regressive
Type reload
Sparky No
Mass Budget
4119.81g TotalCasing (Dry)
1647.0g
40.0%
Propellant
2472.8g
60.0%
Live Sizing
Flight Envelope
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Comparable L-Class Alternatives
BB-75-2500
AMW
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Total: 2590 Ns
Ø 75mm
1685CC098L-L200
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2653L585-P
Cesaroni
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Total: 2653 Ns
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L695BL
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Total: 2669 Ns
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SK-75-3500
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L
neutral
Total: 2700 Ns
Ø 75mm
1685CC172L-L475
Hypertek
L
dual-peak
Total: 2774 Ns
Ø 75mm
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