Template:rocketspecs
{{#if: {{{ref|}}}
|
Data from {{{ref}}}
}}General characteristics
- Type: {{{type|}}}
- Length: {{{length|}}}
- Diameter: {{{diameter|}}}
- Dry weight: {{{weight|}}}
{{#if:{{{capacity|}}}|
- Propellant capacity: {{{capacity|}}}}}
{{#if:{{{fueltype|}}}|
- Fuel: {{{fueltype|}}}}}
{{#if:{{{oxidiser|}}}|
- Oxidiser: {{{oxidiser|}}}}}
Components
- Pumps: {{{pumps|}}}
{{#if:{{{pumps|}}}}}
{{#if:{{{grain|}}}}}
{{#if:{{{core|}}}|
- Core: {{{core|}}}}}
{{#if:{{{casing|}}}|
- Casing: {{{casing|}}}}}
{{#if:{{{combustion_chamber|}}}|
- Combustion chamber: {{{combustion_chamber|}}}}}
{{#if:{{{nozzle|}}}|
- Nozzle: {{{nozzle|}}}}}
{{#if:{{{nozzle_ratio|}}}|
- Nozzle Area ratio: {{{nozzle_ratio|}}}}}
{{#if:{{{cycle|}}}|
- Cycle: {{{cycle|}}}}}
Performance
- Thrust: {{{thrust|}}}
- Burn time: {{{burn_time|}}}
{{#if:{{{thrust|}}}}}
{{#if:{{{thrust/weight|}}}|
- Thrust-to-weight ratio: {{{thrust/weight|}}}}}
{{#if:{{{burn_time|}}}|
- Burn time: {{{burn_time|}}}}}
{{#if:{{{fuelcon|}}}
- Fuel consumption: {{{fuelcon|}}}}}
{{#if:{{{specfuelcon|}}}|
- Thrust specific fuel consumption: {{{specfuelcon|}}}}}
{{#if:{{{thrust(SL)|}}}|
- Thrust(SL): {{{thrust(SL)|}}}
- Power output: {{{power|}}}}}
{{#if:{{{thrust_at_altitude|}}}|
- Thrust (at altitude): {{{thrust_at_altitude|}}}
- Power output: {{{power|}}}}}
{{#if:{{{specific_impulse|}}}|
- Specific impulse: {{{specific_impulse|}}}}}
{{#if:{{{specific_impulse_sea_level|}}}|
- Isp(SL): {{{specific_impulse_sea_level|}}}}}
{{#if:{{{total_impulse|}}}|
- Total impulse: {{{total_impulse|}}}}}