General characteristics
- Crew: {{{crew}}}
- Length: {{{length main}}} ({{{length alt}}})
- Diameter: {{{diameter main}}} ({{{diameter alt}}})
- Wingspan: {{{wingspan main}}} ({{{wingspan alt}}})
- Empty mass: {{{empty mass main}}} ({{{empty mass alt}}})
- Launch mass: {{{launch mass main}}} ({{{launch mass alt}}})
- Payload:
- To low Earth orbit: {{{payload to LEO main}}} ({{{payload to LEO alt}}})
- To the Moon: {{{payload to moon main}}} ({{{payload to moon alt}}})
Engine
- First stage: {{{stage1}}}
- Thrust: {{{thrust1 main}}} ({{{thrust1 alt}}})
- Burn time: {{{burn time1}}}
- Fuel: {{{fuel1}}}
- Second stage: {{{stage2}}}
- Thrust: {{{thrust2 main}}} ({{{thrust2 alt}}})
- Burn time: {{{burn time2}}}
- Fuel: {{{fuel2}}}
- Third stage: {{{stage3}}}
- Thrust: {{{thrust3 main}}} ({{{thrust3 alt}}})
- Burn time:
- Fuel:
or
- {{{engine}}}
- Thrust: {{{thrust main}}} ({{{thrust alt}}})
- Burn time: {{{burn time}}}
- Fuel: {{{fuel}}}
Technical information
- Guidance: {{{guidance}}}
- Launch platform: {{{launch platform}}}
Performance
- Cruise speed: {{{speed main}}} ({{{speed alt}}})
- Operating altitude: {{{altitude main}}} ({{{altitude alt}}})
- Range: {{{range main}}} ({{{range alt}}})
Template documentation