Disclaimer
Important information about using MaxQ analysis tools
Usage Disclaimer
While these tools are built on established aerodynamic and structural analysis methods, they rely on the quality of the input data as well as inherent modeling assumptions. As such, all results are estimates.
The user is ultimately responsible for the design, materials, build quality, launch decision, and flight performance of their rocket.
Modeling Assumptions
- Aerodynamic calculations assume axisymmetric bodies at small angles of attack
- Atmospheric models use standard day conditions which may differ from actual launch conditions
- Structural analysis assumes ideal material properties and construction quality
- Recovery system modeling assumes proper deployment and nominal parachute performance
- Monte Carlo simulations provide statistical estimates, not guarantees
User Responsibilities
- Verify all calculations independently before flight
- Apply appropriate safety margins to all results
- Follow all applicable laws, regulations, and safety codes
- Obtain proper certifications and permissions for high-power rocketry
- Conduct thorough pre-flight inspections and testing
- Make conservative launch decisions based on actual conditions
Limitations of Liability
MaxQ and its developers provide these tools "as is" without warranty of any kind. We are not liable for any damages, injuries, or losses arising from the use of these tools or reliance on their output. Users assume all risks associated with rocket design, construction, and operation.
MaxQ calculations are based on established methods including the Barrowman equations, NACA technical reports, and standard atmospheric models. For critical applications, always consult primary sources and conduct physical testing.