Template:Infobox rocket engine

{	"params": { "name": { "label": "Name", "description": "Name of the rocket engine", "type": "string" },		"image": { "label": "Image", "type": "wiki-file-name", "description": "Filename for image of the rocket engine, do not include the \"File:\" or \"Image:\" prefix" },		"alt": {}, "image_alt": {}, "caption": { "label": "Caption", "description": "Image caption", "type": "string" },		"country_of_origin": { "label": "Country of origin", "type": "string", "description": "Country of origin" },		"date": {}, "first_date": { "label": "First flight date", "description": "Date of the first flight, use ", "example": " ", "type": "string" },		"last_date": { "label": "Last flight date", "description": "Date of the last flight, use ", "example": "", "type": "string" },		"designer": { "label": "Designer", "description": "Designer of the engine, can be linked", "type": "string" },		"manufacturer": { "label": "Manufacturer", "description": "Manufacturer of the engine, can be linked, but do not link if the same as the designer", "type": "string" },		"purpose": {}, "associated": { "label": "Associated launch vehicles", "description": "List of launch vehicles this rocket engine is associated with", "type": "string" },		"predecessor": { "label": "Predecessor ", "description": "Predecessor rocket engine", "type": "string" },		"successor": { "label": "Successor", "description": "Successor rocket engine", "type": "string" },		"status": {}, "type": { "label": "Type", "description": "Type of rocket engine, use liquid, solid, hybrid or mono (for monopropellant) ", "type": "string", "suggestedvalues": [ "liquid", "solid", "hybrid", "mono" ],			"required": true },		"fuel": { "label": "Fuel", "description": "Type of fuel used", "type": "string" },		"oxidizer": { "aliases": [ "oxidiser" ],			"label": "Oxidizer", "description": "Type of oxidizer used", "type": "string" },		"grain": {}, "core": {}, "casing": {}, "nozzle": {}, "mixture_ratio": {}, "cycle": {}, "pumps": {}, "combustion_chamber": {}, "nozzle_ratio": {}, "description": {}, "thrust(Vac)": { "label": "Thrust, vacuum", "description": "Thrust of the engine, in vacuum, use VALUEHERE kN", "example": "VALUEHERE kN", "type": "string" },		"thrust(SL)": { "label": "Thrust, sea level", "description": "Thrust of the engine, at sea level, use VALUEHERE kN", "example": "VALUEHERE kN", "type": "string" },		"thrust": { "label": "Thrust", "deprecated": "Use Thrust, vacuum or Thrust, sea level" },		"thrust_at_altitude": {}, "thrust_to_weight": {}, "chamber_pressure": {}, "specific_impulse": { "label": "Specific impulse", "deprecated": "Use Specific impulse, vacuum or Specific impulse, sea level" },		"specific_impulse_vacuum": { "label": "Specific impulse, vacuum", "description": "Specific impulse of the engine, in vacuum, use VALUEHERE isp", "example": "VALUEHERE isp", "type": "string" },		"specific_impulse_sea_level": { "label": "Specific impulse, vacuum", "description": "Specific impulse of the engine, at sea level, use VALUEHERE isp", "example": "VALUEHERE isp" },		"total_impulse": {}, "burn_time": { "label": "Burn time", "description": "The length of time the engine burns normally, in seconds", "example": "NNN seconds", "type": "string" },		"capacity": {}, "throttle_range": {}, "mass_flow": {}, "restarts": { "label": "Restarts", "description": "How many times the engine can be restarted, leave blank if not restartable" },		"gimbal": { "label": "Gimbal range", "description": "Gimbal range in °, leave blank if none-->", "example": "NN°", "type": "string" },		"dimensions": {}, "length": { "label": "Length", "description": "Length of the engine, in metres, use VALUE m", "example": "VALUE m", "type": "string" },		"diameter": { "label": "Diameter", "description": "Diameter of the engine at widest part (typically nozzle tip), in metres, use VALUE m", "example": "VALUE m", "type": "string" },		"dry_weight": { "label": "Dry weight", "description": "Mass of unfueled rocket engine in kilograms, use MASS kg", "example": "MASS kg", "type": "string" },		"used_in": {}, "embedded": {}, "module": {}, "references": {}, "notes": {}, "image_size": { "aliases": [ "imsize" ],			"label": "Image size", "description": "Image size in pixels", "type": "string" }	},	"format": "", "paramOrder": [ "name", "image", "image_size", "alt", "image_alt", "caption", "country_of_origin", "date", "first_date", "last_date", "designer", "manufacturer", "purpose", "associated", "predecessor", "successor", "status", "type", "fuel", "oxidizer", "grain", "core", "casing", "nozzle", "mixture_ratio", "cycle", "pumps", "combustion_chamber", "nozzle_ratio", "description", "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", "throttle_range", "mass_flow", "restarts", "gimbal", "dimensions", "length", "diameter", "dry_weight", "used_in", "embedded", "module", "references", "notes" ] }