1st stage average trajectory Isp |
s |

1st stage delta-v |
m/s |

1st stage final mass |
kg |

1st stage propellant mass |
kg |

1st stage dry mass |
kg |

1st stage total thrust |
kgf |

1st stage engines run time |
s |

1st stage Maximum Acceleration |
g |

2nd stage delta-v |
m/s |

2nd stage total (start) mass |
kg |

2nd stage total mass before fairing jettison |
kg |

2nd stage total mass before battery jettison |
kg |

2nd stage delta-v before batt. jettison |
m/s |

2nd stage final mass |
kg |

2nd stage propellant mass |
kg |

2nd stage dry mass |
kg |

2nd stage total thrust |
kgf |

2nd stage engine run time |
s |

2nd stage Maximum Acceleration |
g |

Transfer Orbit stage delta-v (required) |
m/s |

Transfer Orbit stage total (start) mass |
kg |

Transfer Orbit stage final mass |
kg |

Transfer Orbit stage propellant mass |
kg |

Transfer Orbit stage dry mass |
kg |

Calculation Error |
m/s |