N Class Rocket Motor

AeroTech N3300R

AeroTech
Redline
Ø 98mm
Total Impulse
14041.0Ns
Burn Time
4.37s
Avg Thrust
3168.0N
Max Thrust
4301.0N

Thrust Profile (N)

4.37s Burn Window

Engineered by AeroTech, the N3300R is a 98mm solid rocket motor designed for extreme high-power rocketry. As an official N-class motor, it delivers a total impulse of 14041.0 Ns over a 4.37 second burn window.

With an average thrust of 3168.0 N and a peak of 4301.0 N, it features a regressive thrust curve optimal for sustainer stages and high-altitude attempts. It utilizes the Redline propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 98 mm
Length 1046 mm
Hardware RMS-98/15360
Delays (s) P
Specific Impulse 190.5 s
Peak Thrust 3775.78 N
Peak Time T+ 0.125s
T/W Ratio 26.79
Propellant Redline
Profile regressive
Type reload
Sparky No

Mass Budget

12054g Total
Casing (Dry)
4542.0g
37.7%
Propellant
7512.0g
62.3%
Live Sizing
Flight Envelope

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Comparable N-Class Alternatives

WT-98-11000

AMW

N
neutral
Total: 10281 Ns
Ø 98mm

10347N10000-P

Cesaroni

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neutral
Total: 10347 Ns
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10367N1800-P

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N
regressive
Total: 10367 Ns
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GG-98-11000

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N
neutral
Total: 10607 Ns
Ø 98mm

N2220DM

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N
regressive
Total: 10657 Ns
Ø 98mm

N2717WC

Gorilla

N
neutral
Total: 10813 Ns
Ø 98mm
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