L Class Rocket Motor

Contrail L1222-SM

Contrail Rockets
Unknown
Ø 75mm
Total Impulse
3682.0Ns
Burn Time
3.10s
Avg Thrust
1173.0N
Max Thrust
2892.0N

Thrust Profile (N)

3.10s Burn Window

Engineered by Contrail Rockets, the L1222-SM is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official L-class motor, it delivers a total impulse of 3682.0 Ns over a 3.10 second burn window.

With an average thrust of 1173.0 N and a peak of 2892.0 N, it features a neutral thrust curve optimal for heavy rockets requiring high off-the-pad acceleration.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 75 mm
Length 1371 mm
Hardware 75x1524 (3200CC)
Delays (s) P
Specific Impulse 477.5 s
Peak Thrust 2725 N
Peak Time T+ 0.5s
T/W Ratio 23.97
Propellant Standard
Profile neutral
Type hybrid
Sparky Yes

Mass Budget

4989g Total
Casing (Dry)
4203.0g
84.2%
Propellant
786.0g
15.8%
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.

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.

Loading calendar...