rocket_deltav
Aerospace & orbital mechanics: calculate Tsiolkovsky rocket equation delta-v budget, mass ratio, and propellant consumption.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| gravityMs2 | No | Standard gravity g0 in m/s^2 | |
| finalMassKg | Yes | Dry burnout mass mf in kg | |
| initialMassKg | Yes | Wet launch mass m0 in kg | |
| specificImpulseSeconds | Yes | Engine specific impulse Isp in seconds |