H Class Rocket Motor

AeroTech HP-H182R

AeroTech
Redline
Ø 29mm
Total Impulse
218.0Ns
Burn Time
1.20s
Avg Thrust
182.0N
Max Thrust
192.0N

Thrust Profile (N)

1.20s Burn Window

Engineered by AeroTech, the HP-H182R is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 218.0 Ns over a 1.20 second burn window.

With an average thrust of 182.0 N and a peak of 192.0 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 29 mm
Length 203 mm
Hardware Single Use
Delays (s) 6,8,10,12,14
Specific Impulse 193.2 s
Peak Thrust 200.81 N
Peak Time T+ 1.144s
T/W Ratio 89.63
Propellant Redline
Profile dual-peak
Type SU
Sparky No

Mass Budget

207g Total
Casing (Dry)
92.0g
44.4%
Propellant
115.0g
55.6%
Live Sizing
Flight Envelope

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Comparable H-Class Alternatives

H155F

Kosdon

H
dual-peak
Total: 161 Ns
Ø 29mm

H300-HP

Contrail

H
neutral
Total: 161 Ns
Ø 38mm

H222-HP

Contrail

H
regressive
Total: 161 Ns
Ø 38mm

H55W

AeroTech

H
regressive
Total: 162 Ns
Ø 29mm

163H133-14A

Cesaroni

H
dual-peak
Total: 163 Ns
Ø 29mm

164H90-12A

Cesaroni

H
dual-peak
Total: 164 Ns
Ø 29mm
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