M Class Rocket Motor

AeroTech M2000R

AeroTech
Redline
Ø 98mm
Total Impulse
9218.0Ns
Burn Time
4.00s
Avg Thrust
2000.0N
Max Thrust
2327.0N

Thrust Profile (N)

4.00s Burn Window

Engineered by AeroTech, the M2000R is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 9218.0 Ns over a 4.00 second burn window.

With an average thrust of 2000.0 N and a peak of 2327.0 N, it features a dual-peak thrust curve optimal for general sport flying. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 98 mm
Length 732 mm
Hardware RMS-98/10240
Delays (s) P
Specific Impulse 175 s
Peak Thrust 2316.16 N
Peak Time T+ 1.974s
T/W Ratio 22.69
Propellant Redline
Profile dual-peak
Type reload
Sparky No

Mass Budget

8986.88g Total
Casing (Dry)
3618.9g
40.3%
Propellant
5368.0g
59.7%
Live Sizing
Flight Envelope

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