M Class Rocket Motor

AeroTech M2050X-P

AeroTech
Propellant X
Ø 75mm
Total Impulse
5493.4Ns
Burn Time
2.70s
Avg Thrust
2047.6N
Max Thrust
2544.2N

Thrust Profile (N)

2.70s Burn Window

Engineered by AeroTech, the M2050X-P is a 75mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 5493.4 Ns over a 2.70 second burn window.

With an average thrust of 2047.6 N and a peak of 2544.2 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Propellant X propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 75 mm
Length 699.7 mm
Hardware RMS-75/5120
Delays (s) P
Specific Impulse 246.9 s
Peak Thrust 2562.08 N
Peak Time T+ 0.067s
T/W Ratio 45.79
Propellant Propellant X
Profile regressive
Type reload
Sparky No

Mass Budget

4558.6g Total
Casing (Dry)
2290.6g
50.2%
Propellant
2268.0g
49.8%
Live Sizing
Flight Envelope

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Comparable M-Class Alternatives

M1200-SF

Loki

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neutral
Total: 5123 Ns
Ø 76mm

2800CC300MFX-M960FX

Hypertek

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Total: 5126 Ns
Ø 75mm

2800CC200M-M740

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Total: 5143 Ns
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M1355RT

Gorilla

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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
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