109.70.40.55 at 14:47, 17 January 2022

2022-01-17T14:47:34Z

New page

{{Infobox
| title = <includeonly>{{{name|{{PAGENAMEBASE}}}}}</includeonly>
| headerstyle = background-color:#FFDEAD
| image = {{#invoke:InfoboxImage|InfoboxImage|image={{{image|}}}|size={{{image_size|{{{imsize|}}}}}}|sizedefault=frameless|upright=1.13|alt={{{alt|{{{image_alt|}}}}}}}}
| caption = {{{caption|}}}

| label1 = Country of origin
| data1 = {{{country_of_origin|}}}

| label2 = Date
| data2 = {{{date|}}}

| label3 = First flight
| data3 = {{{first_date|}}}

| label4 = Last flight
| data4 = {{{last_date|}}}

| label5 = Designer
| data5 = {{{designer|}}}

| label10 = Manufacturer
| data10 = {{{manufacturer|}}}

| label11 = Application
| data11 = {{{purpose|}}}

| label12 = Associated {{abbr|LV|launch vehicle}}
| data12 = {{{associated|}}}

| label13 = Predecessor
| data13 = {{{predecessor|}}}

| label14 = Successor
| data14 = {{{successor|}}}

| label15 = Status
| data15 = {{{status|}}}

| header20 = {{#switch: {{lc:{{{type|}}}}}
| solid = [[Solid-fuel rocket|Solid-fuel motor]]
| liquid = [[Liquid-propellant rocket|Liquid-fuel engine]]
| hybrid = [[Hybrid rocket|Hybrid engine]]
| mono|monopropellant = {{{fuel|}}} [[monopropellant]]
| #default = {{{type|}}}
}}


| label21 = Propellant
| data21 = {{#switch: {{lc:{{{type|}}}}}
| solid
| liquid
| hybrid = {{#if: {{{oxidizer|}}}{{{oxidiser|}}} | {{{oxidizer|{{{oxidiser|}}}}}} / }} {{{fuel|}}}
}}



| label22 = Grain
| data22 = {{#ifeq:{{{type|}}}|solid| {{{grain|}}} }}

| label23 = Core
| data23 = {{#ifeq:{{{type|}}}|solid| {{{core|}}} }}

| label24 = Casing
| data24 = {{#ifeq:{{{type|}}}|solid| {{{casing|}}} }}

| label25 = Nozzle
| data25 = {{#ifeq:{{{type|}}}|solid| {{{nozzle|}}} }}



| label30 = Mixture ratio
| data30 = {{#ifeq:{{{type|}}}|liquid| {{{mixture_ratio|}}} }}

| label31 = Cycle
| data31 = {{#ifeq:{{{type|}}}|liquid| {{{cycle|}}} }}

| label32 = Pumps
| data32 = {{#ifeq:{{{type|}}}|liquid| {{{pumps|}}} }}


| header40 = {{#if: {{{combustion_chamber|}}}{{{nozzle_ratio|}}} | Configuration }}

| data41 = {{{description|}}}

| label42 = Chamber
| data42 = {{{combustion_chamber|}}}

| label43 = Nozzle ratio
| data43 = {{{nozzle_ratio|}}}

| header50 = {{#if: {{{thrust(Vac)|}}}{{{thrust(SL)|}}}{{{thrust|}}}{{{thrust_at_altitude|}}}{{{thrust_to_weight|}}}{{{chamber_pressure|}}}{{{specific_impulse|}}}{{{specific_impulse_vacuum|}}}{{{specific_impulse_sea_level|}}}{{{total_impulse|}}}{{{burn_time|}}}{{{capacity|}}} | Performance }}

| label51 = Thrust
| data51 = {{{thrust|}}}

| label52 = {{#if: {{{thrust|}}} |     at altitude | Thrust, at altitude }}
| data52 = {{{thrust_at_altitude|}}}

| label53 = Thrust, vacuum
| data53 = {{{thrust(Vac)|}}}

| label54 = Thrust, sea-level
| data54 = {{{thrust(SL)|}}}

| label55 = Throttle range
| data55 = {{{throttle_range|}}}

| label60 = [[Thrust-to-weight ratio]]
| data60 = {{{thrust_to_weight|}}}

| label61 = Chamber [[pressure]]
| data61 = {{{chamber_pressure|}}}

| label62 = [[Specific impulse]]
| data62 = {{{specific_impulse|}}}

| label63 = [[Specific impulse]], vacuum
| data63 = {{{specific_impulse_vacuum|}}}

| label64 = [[Specific impulse]], sea-level
| data64 = {{{specific_impulse_sea_level|}}}

| label65 = [[Impulse (physics)|Total impulse]]
| data65 = {{{total_impulse|}}}

| label66 = [[Mass flow rate|Mass flow]]
| data66 = {{{mass_flow|}}}

| label70 = Burn time
| data70 = {{{burn_time|}}}

| label71 = Restarts
| data71 = {{{restarts|}}}

| label72 = {{#switch: {{lc:{{{type|}}}}}
| solid = [[Thrust vectoring]]
| liquid = [[Gimbaled thrust|Gimbal range]]
| hybrid = [[Thrust vectoring]]
| mono
| monopropellant = [[Gimbaled thrust|Gimbal range]]
}}

| data72 = {{{gimbal|}}}

| label73 = Propellant capacity
| data73 = {{{capacity|}}}

| header80 = {{#if: {{{dimensions|}}}{{{length|}}}{{{diameter|}}}{{{dry_weight|}}} | Dimensions }}

| label81 = Measurement
| data81 = {{{dimensions|}}}

| label82 = Length
| data82 = {{{length|}}}

| label83 = Diameter
| data83 = {{{diameter|}}}

| label84 = Dry weight
| data84 = {{{dry_weight|}}}
| header90 = {{#if: {{{used_in|}}} | Used in }}
| data91 = {{{used_in|}}}

| header99 = {{{embedded|{{{module|}}}}}}

| header100 = {{#if: {{{references|}}}{{{notes|}}} | References }}

| label101 = References
| data101 = {{{references|}}}

| label102 = Notes
| data102 = {{{notes|}}}

}}{{main other|
{{#switch: {{lc:{{{country_of_origin|}}}}}
| britain|uk|united kingdom = [[Category:Rocket engines of the United Kingdom]]
| russia|russian|soviet|soviet union = [[Category:Rocket engines of the Soviet Union]]
| us|usa|united states = 
| france = 
}}{{#switch: {{lc:{{{type|}}}}}
| mono|monopropellant = [[Category:Monopropellant rocket engines]]
| solid = 
| liquid = 
| hybrid = 
}}
}}<noinclude>
{{Documentation}}
</noinclude>

Template:Infobox rocket engine - Revision history

109.70.40.55 at 14:47, 17 January 2022