M Class Rocket Motor

Cesaroni 8634M6400-P

Cesaroni Technology
Vmax
Ø 98mm
Total Impulse
8634.4Ns
Burn Time
1.36s
Avg Thrust
6365.2N
Max Thrust
7237.8N

Thrust Profile (N)

1.36s Burn Window

Engineered by Cesaroni Technology, the 8634M6400-P is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official M-class motor, it delivers a total impulse of 8634.4 Ns over a 1.36 second burn window.

With an average thrust of 6365.2 N and a peak of 7237.8 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Vmax propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Canadian Association of Rocketry
Diameter 98 mm
Length 702 mm
Hardware Pro98-4G
Delays (s) P
Specific Impulse 210.8 s
Peak Thrust 7244.6 N
Peak Time T+ 0.503s
T/W Ratio 81.94
Propellant Vmax
Profile neutral
Type reload
Sparky No

Mass Budget

7919g Total
Casing (Dry)
3744.0g
47.3%
Propellant
4175.0g
52.7%
Live Sizing
Flight Envelope

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Comparable M-Class Alternatives

5342M1560-P

Cesaroni

M
dual-peak
Total: 5342 Ns
Ø 98mm

M1075DM

AeroTech

M
neutral
Total: 5571 Ns
Ø 98mm

M2700-BS

Contrail

M
dual-peak
Total: 6034 Ns
Ø 98mm

M2800-BG

Contrail

M
neutral
Total: 6060 Ns
Ø 98mm

M845H

AeroTech

M
regressive
Total: 6159 Ns
Ø 98mm

3500CCRGMFX-M1015FX

Hypertek

M
regressive
Total: 6334 Ns
Ø 98mm
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