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.

Google Sheets Install in Google Sheets coming soon
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...