H Class Rocket Motor

AeroTech H169WS-13

AeroTech
Super White Lightning
Ø 29mm
Total Impulse
232.9Ns
Burn Time
1.38s
Avg Thrust
168.8N
Max Thrust
231.4N

Thrust Profile (N)

1.38s Burn Window

Engineered by AeroTech, the H169WS-13 is a 29mm solid rocket motor designed for high-power rocketry (HPR). As an official H-class motor, it delivers a total impulse of 232.9 Ns over a 1.38 second burn window.

With an average thrust of 168.8 N and a peak of 231.4 N, it features a neutral thrust curve optimal for general sport flying. It utilizes the Super White Lightning propellant formulation, dictating its specific impulse and exhaust signature.

Technical Specifications

Tripoli Rocketry Association, Inc.
Diameter 29 mm
Length 220.70000000000002 mm
Hardware Single Use
Delays (s) 5,7,9,11,13
Specific Impulse 212 s
Peak Thrust 233.46 N
Peak Time T+ 0.22s
T/W Ratio 85.1
Propellant Super White Lightning
Profile neutral
Type SU
Sparky No

Mass Budget

202.2g Total
Casing (Dry)
90.2g
44.6%
Propellant
112.0g
55.4%
Live Sizing
Flight Envelope

Design wings in your spreadsheet

AeroSheet loads airfoils directly into Google Sheets. Polars, 3D splines, Fusion 360 export, without leaving your spreadsheet.

Google Sheets Install in Google Sheets coming soon
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
Veenie Kit

Need a custom engineering simulator?

The 3D engine on this page is built by Veenie Aerospace. We build bespoke, browser-native digital twins, aerodynamic simulators, and AI physics tools for UAV startups and defense contractors.

ivan@veenie.space
Loading calendar...
ivan@veenie.space