Template:Jetspecs

{{#if: {{{ref|}}}

|

Data from {{{ref}}}

}}

General characteristics

• Type: {{{type|}}}
• Length: {{{length|}}}
• Diameter: {{{diameter|}}}
• Dry weight: {{{weight|}}}

Components

• Compressor: {{{compressor|}}}{{#if:{{{combustion|}}}

|* Combustors: {{{combustion|}}}

}}{{#if:{{{turbine|}}}

|* Turbine: {{{turbine|}}}

}}{{#if:{{{fueltype|}}}

|* Fuel type: {{{fueltype|}}}

}}{{#if:{{{oilsystem|}}}

|* Oil system: {{{oilsystem|}}}

}}

Performance

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

|* Maximum thrust: {{{thrust|}}}

|* Maximum power output: {{{power|}}}

}}{{#if:{{{compression|}}}

|* Overall pressure ratio: {{{compression|}}}

}}{{#if:{{{bypass|}}}

|* Bypass ratio: {{{bypass|}}}

}}{{#if:{{{airflow|}}}

|* Air consumption: {{{airflow|}}}

}}{{#if:{{{aircon|}}}

|* Air mass flow: {{{aircon|}}}

}}{{#if:{{{turbinetemp|}}}

|* Turbine inlet temperature: {{{turbinetemp|}}}

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

|* Fuel consumption: {{{fuelcon|}}}

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

|* Specific fuel consumption: {{{specfuelcon|}}}

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

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

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

|* Power-to-weight ratio: {{{power/weight|}}}

}}

{{documentation}}