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
Design wings in your spreadsheet
AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.
Install in Google Sheets coming soon Comparable L-Class Alternatives
BB-75-2500
AMW
L
neutral
Total: 2590 Ns
Ø 75mm
1685CC098L-L200
Hypertek
L
regressive
Total: 2639 Ns
Ø 75mm
2653L585-P
Cesaroni
L
dual-peak
Total: 2653 Ns
Ø 75mm
L695BL
Gorilla
L
neutral
Total: 2669 Ns
Ø 75mm
SK-75-3500
AMW
L
neutral
Total: 2700 Ns
Ø 75mm
1685CC172L-L475
Hypertek
L
dual-peak
Total: 2774 Ns
Ø 75mm
Veenie Kit
Need a custom engineering simulator?
The 3D engine on this page is built by Veenie Aerospace. We build bespoke, browser-native digital twins, aerodynamic simulators, and AI physics tools for UAV startups and defense contractors.