M Class Rocket Motor

Loki M1200-SF

Loki Research
Spitfire
Ø 76mm
Total Impulse
5122.6Ns
Burn Time
4.49s
Avg Thrust
1241.6N
Max Thrust
1550.0N

Thrust Profile (N)

4.49s Burn Window

Engineered by Loki Research, the M1200-SF is a 76mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 5122.6 Ns over a 4.49 second burn window.

With an average thrust of 1241.6 N and a peak of 1550.0 N, it features a neutral thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Spitfire propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 76 mm
Length 785 mm
Hardware 76/6000
Delays (s) P
Specific Impulse 175.9 s
Peak Thrust 1514.51 N
Peak Time T+ 2s
T/W Ratio 23.58
Propellant Spitfire
Profile neutral
Type reload
Sparky Yes

Mass Budget

5368g Total
Casing (Dry)
2400.0g
44.7%
Propellant
2968.0g
55.3%
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
Comparable M-Class Alternatives

2800CC300MFX-M960FX

Hypertek

M
regressive
Total: 5126 Ns
Ø 75mm

2800CC200M-M740

Hypertek

M
regressive
Total: 5143 Ns
Ø 75mm

M1355RT

Gorilla

M
neutral
Total: 5165 Ns
Ø 75mm

M1350W

AeroTech

M
dual-peak
Total: 5178 Ns
Ø 75mm

5198M1101-P

Cesaroni

M
dual-peak
Total: 5198 Ns
Ø 75mm

M2225WS

AeroTech

M
dual-peak
Total: 5205 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.

ivan@veenie.space
Loading calendar...
ivan@veenie.space