M Class Rocket Motor

AeroTech M1600R

AeroTech
Redline
Ø 98mm
Total Impulse
7084.0Ns
Burn Time
4.00s
Avg Thrust
1600.0N
Max Thrust
1917.0N

Thrust Profile (N)

4.00s Burn Window

Engineered by AeroTech, the M1600R is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 7084.0 Ns over a 4.00 second burn window.

With an average thrust of 1600.0 N and a peak of 1917.0 N, it features a neutral 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 579 mm
Hardware RMS-98/7680
Delays (s) P
Specific Impulse 179.4 s
Peak Thrust 1856.37 N
Peak Time T+ 1.529s
T/W Ratio 23.58
Propellant Redline
Profile neutral
Type reload
Sparky No

Mass Budget

6917.12g Total
Casing (Dry)
2891.1g
41.8%
Propellant
4026.0g
58.2%
Live Sizing
Flight Envelope

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