Template:Rocketspecs/sandbox

Testing location

Put the template code here and experiment with it.

Put your test example at Template:Rocketspecs/testcases

And there use

{{Rocketspecs/sandbox

|param=

|param=

|etc

}}

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

{{#if:{{{thrust|}}}|

• Thrust: {{{thrust|}}}}}

  {{#if:{{{thrust/weight|}}}|

• Thrust-to-weight ratio: {{{thrust/weight|}}}}}

  {{#if:{{{burn time|}}}|

• Burn time: {{{burn time|}}}}}

  {{#if:{{{fuelcon|}}}|

• Fuel consumption: {{{fuelcon|}}}}}

  {{#if:{{{specfuelcon|}}}|

• 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|}}}|

• I_sp(SL): {{{specific_impulse_sea_level|}}}}}

  {{#if:{{{total_impulse|}}}|

• Total impulse: {{{total_impulse|}}}}}

{{esoteric}}

This template provides formatted output for aircraft rocket engine specifications per Wikipedia:WikiProject Aircraft/page content. To use this template, copy-paste the following text:

{{rocketspecs

|ref=

|type=

|length=

|diameter=

|weight=

|fueltype=

|oxidiser=

|capacity=

|pumps=

|thrust=

|thrust/weight=

|burn time=

|fuelcon=

|specfuelcon=

}}

See Template talk:Jettemp for explanation of parameters.