Template:Aircraft specs/testcases
{{Template test cases notice}}
One of everything
= (fictional metric)=
{{testcase table
|ref=source name
|prime units?=met
|genhide=
|crew=one pilot
|capacity=lots of passengers
|length m=20
|length ft=
|length in=
|length note=nose probe to tail light
|span m=30
|span ft=
|span in=
|span note=with extra tips
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=5
|height ft=
|height in=
|height note=to top of rudder
|wing area sqm=
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=NACA something
|empty weight kg=5000
|empty weight lb=
|empty weight note=absolutely dry
|gross weight kg=7500
|gross weight lb=
|gross weight note=all up
|max takeoff weight kg=7800
|max takeoff weight lb=
|max takeoff weight note=if you must
|fuel capacity=1500 litres
|lift kg=
|lift lb=
|lift note=
|more general=
- Extra note: something else
|eng1 number=4
|eng1 name=Rolls-Whitney AS5
|eng1 type=turbines
|eng1 kw=
|eng1 hp=
|eng1 shp=
|eng1 kn=5000
|eng1 lbf=
|eng1 note=at full power
|power original=
|thrust original=
|eng1 kn-ab=1500
|eng1 lbf-ab=
|eng2 number=
|eng2 name=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 shp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 shp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=
|perfhide=
|max speed kmh=500
|max speed mph=
|max speed kts=
|max speed note=flat out
|max speed mach=
|cruise speed kmh=350
|cruise speed mph=
|cruise speed kts=
|cruise speed note=nice and gentle
|stall speed kmh=160
|stall speed mph=
|stall speed kts=
|stall speed note=full flaps and praying
|never exceed speed kmh=800
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=on a good day
|minimum control speed kmh=155
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=whatever this means
|range km=1000
|range miles=
|range nmi=
|range note=full tank
|combat range km=500
|combat range miles=
|combat range nmi=
|combat range note=travelling light
|ferry range km=2000
|ferry range miles=
|ferry range nmi=
|ferry range note=with extra tanks
|endurance=
|ceiling m=10000
|ceiling ft=
|ceiling note=half full
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=10
|climb rate ftmin=
|climb rate note=kind of gentle
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=22
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|armament=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}
= (fictional imp)=
but with only metric values in the params
{{testcase table
|ref=source name
|prime units?=imp
|genhide=
|crew=one pilot
|capacity=lots of passengers
|length m=20
|length ft=
|length in=
|length note=nose probe to tail light
|span m=30
|span ft=
|span in=
|span note=with extra tips
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=5
|height ft=
|height in=
|height note=to top of rudder
|wing area sqm=
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=NACA something
|empty weight kg=5000
|empty weight lb=
|empty weight note=absolutely dry
|gross weight kg=7500
|gross weight lb=
|gross weight note=all up
|max takeoff weight kg=7800
|max takeoff weight lb=
|max takeoff weight note=if you must
|fuel capacity=1500 litres
|lift kg=
|lift lb=
|lift note=
|more general=
- Extra note: something else
|eng1 number=4
|eng1 name=Rolls-Whitney AS5
|eng1 type=turbines
|eng1 kw=
|eng1 hp=
|eng1 shp=
|eng1 kn=5000
|eng1 lbf=
|eng1 note=at full power
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 name=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 shp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 shp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=
|perfhide=
|max speed kmh=500
|max speed mph=
|max speed kts=
|max speed note=flat out
|max speed mach=
|cruise speed kmh=350
|cruise speed mph=
|cruise speed kts=
|cruise speed note=nice and gentle
|stall speed kmh=160
|stall speed mph=
|stall speed kts=
|stall speed note=full flaps and praying
|never exceed speed kmh=800
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=on a good day
|minimum control speed kmh=155
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=whatever this means
|range km=1000
|range miles=
|range nmi=
|range note=full tank
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=10000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=10
|climb rate ftmin=
|climb rate note=kind of gentle
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=22
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|armament=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}
= (fictional in knots)=
but only metric in params
{{testcase table
|ref=source name
|prime units?=kts
|genhide=
|crew=one pilot
|capacity=lots of passengers
|length m=20
|length ft=
|length in=
|length note=nose probe to tail light
|span m=30
|span ft=
|span in=
|span note=with extra tips
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=5
|height ft=
|height in=
|height note=to top of rudder
|wing area sqm=
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=NACA something
|empty weight kg=5000
|empty weight lb=
|empty weight note=absolutely dry
|gross weight kg=7500
|gross weight lb=
|gross weight note=all up
|max takeoff weight kg=7800
|max takeoff weight lb=
|max takeoff weight note=if you must
|fuel capacity=1500 litres
|lift kg=
|lift lb=
|lift note=
|more general=
- Extra note: something else
|eng1 number=4
|eng1 name=Rolls-Whitney AS5
|eng1 type=turbines
|eng1 kw=
|eng1 hp=
|eng1 shp=
|eng1 kn=5000
|eng1 lbf=
|eng1 note=at full power
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 name=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 shp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 shp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=
|perfhide=
|max speed kmh=500
|max speed mph=
|max speed kts=
|max speed note=flat out
|max speed mach=
|cruise speed kmh=350
|cruise speed mph=
|cruise speed kts=
|cruise speed note=nice and gentle
|stall speed kmh=160
|stall speed mph=
|stall speed kts=
|stall speed note=full flaps and praying
|never exceed speed kmh=800
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=on a good day
|minimum control speed kmh=155
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=whatever this means
|range km=1000
|range miles=
|range nmi=
|range note=full tank
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=10000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=10
|climb rate ftmin=
|climb rate note=kind of gentle
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=22
|fuel consumption lb/mi=23
|power/mass=
|thrust/weight=
|more performance=*Something else: but nothing special
|armament=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}
Testing auto reversing (MET, no inches)
{{testcase table
|ref=
|prime units?=met
|genhide=
|crew=
|capacity=
|length m=2
|length ft=
|length in=
|length note=
|span m=
|span ft=2
|span in=
|span note=
|upper span m=
|upper span ft=2
|upper span in=
|upper span note=
|mid span m=
|mid span ft=2
|mid span in=
|mid span note=
|lower span m=
|lower span ft=2
|lower span in=
|lower span note=
|swept m=
|swept ft=2
|swept in=
|swept note=
|dia m=
|dia ft=2
|dia in=
|dia note=
|width m=
|width ft=2
|width in=
|width note=
|height m=
|height ft=2
|height in=
|height note=
|wing area sqm=
|wing area sqft=2
|wing area note=
|swept area sqm=
|swept area sqft=2
|swept area note=
|volume m3=
|volume ft3=2
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=2
|empty weight note=
|gross weight kg=
|gross weight lb=2
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=2
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=2
|lift note=
|more general=
|eng1 number=1
|eng1 name=x
|eng1 type=y
|eng1 kw=
|eng1 hp=2
|eng1 kn=
|eng1 lbf=2
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=2
|eng2 number=2
|eng2 name=v
|eng2 type=f
|eng2 kw=
|eng2 hp=2
|eng2 kn=
|eng2 lbf=2
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=2
|eng3 number=3
|eng3 name=f
|eng3 type=g
|eng3 kw=
|eng3 hp=2
|eng3 kn=
|eng3 lbf=2
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=2
|more power=
|prop blade number=2
|prop name=sds
|prop dia m=
|prop dia ft=2
|prop dia in=
|prop note=
|rot number=3
|rot dia m=
|rot dia ft=2
|rot dia in=
|rot area sqm=
|rot area sqft=2
|rot area note=
|perfhide=
|max speed kmh=
|max speed mph=2
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=2
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=2
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=2
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=2
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=2
|range nmi=
|range note=
|combat range km=
|combat range miles=2
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=2
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=2
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=2
|climb rate note=
|sink rate ms=
|sink rate ftmin=2
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=2
|wing loading note=
|disk loading kg/m2
|disk loading lb/sqft=2
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=2
|power/mass=
|thrust/weight=
}}
Specifications
{{testcase table
|ref=British Civil Aircraft 1919-72Jackson 1973 p.296
|prime units?=met
|genhide=
|crew=2
|capacity=
|length m=4
|length ft=22
|length in=3.5
|span m=7
|span ft=27
|span in=4
|span note=overall
|lower span ft=27
|lower span in=4
|upper span m=6
|upper span ft=22
|upper span in=0
|height m=
|height ft=
|height in=
|wing area sqm=5
|wing area note=excluding ailerons
|wing area sqft=164
|airfoil=modified RAF31something else
|empty weight kg=200
|empty weight lb=480
|gross weight kg=400
|gross weight lb=874
|more general=
|eng1 number=1
|eng1 name=Bristol Cherub III
|eng1 type=flat twin piston engine
|eng1 kw=
|eng1 hp=
|power original=
|thrust original=
|more power=
|prop type=2 bladed wooden propeller
|prop dia m=2
|props per engine=1
|prop note=ref goes here
|perfhide=
|max speed kmh=
|max speed mph=65
|max speed kts=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|range km=
|range miles=
|range nmi=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|lift to drag=
|wing loading=
|disk loading=
|more performance=
|avionics=
}}
{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}
prop testing section
=no number value test=
{{testcase table
|ref=
|prime units?=met
|prop type=6 bladed contra-rotating
|prop dia m=1
|props per engine=
|prop note=(note b)
}}
=diameter test=
{{testcase table
|ref=
|prime units?=met
|prop type=2 bladed wooden propeller
|prop dia m=
|props per engine=1
|prop note=(Model A only)
}}
=type test=
{{testcase table
|ref=
|prime units?=met
|prop type=4 bladed Rotol reversing propeller
|prop dia m=2.4
|props per engine=2
|prop note=something
}}
=type test=
{{testcase table
|ref=
|prime units?=met
|prop name=Rotol reversing propeller
}}
{{testcase table
|ref=
|prime units?=met
|prop blade number=317
|prop name=Rotol reversing propeller
}}
Rotodyne
{{testcase table
|ref=
|prime units?=imp
|genhide=
|crew=2
|capacity=48 passengers
|length m=
|length ft=58
|length in=8
|length note=
|span m=
|span ft=90
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=
|height ft=22
|height in=2
|height note=
|wing area sqm=
|wing area sqft=6360
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=33000
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=38000
|max takeoff weight note=
|lift kg=
|lift lb=
|lift note=
|more general=
|eng1 number=4
|eng1 name=rotor tip jet
|eng1 type= burning compressed air/fuel
|eng1 kw=
|eng1 hp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=2
|eng2 name=Napier Eland
|eng2 type=turboprop
|eng2 kw=
|eng2 hp=2800
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|rot number=1
|rot dia m=
|rot dia ft=90
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=
|perfhide=
|max speed kmh=
|max speed mph=213
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=520
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=5.2
|disk loading note=
|more performance=
- Power/mass (prop): {{convert|0.17|hp/lb|abbr=on}}
|power/mass met=
|power/mass note=
|thrust/weight met=
|thrust/weight note=
}}
Embedded lists with extra information
{{testcase table
|ref=astronautix.com
|prime units?=imp
|crew=One
|length m=5
|span m=5
|dia m=1.52
|wing area sqm=15
|empty weight kg=1200
|gross weight kg=3600
|more general=
- Aspect Ratio: 1.6
|eng1 number=1
|eng1 type=hybrid rocket
|eng1 kn=73.5
|more power=
- Isp: {{cvt|250|s}}
- Burn time: 80 seconds
|perfhide=
|max speed mach=3.09 (2370 mph, 3815 kph)
|range km=65
|ceiling m=112000
|climb rate ftmin=82000
|wing loading kg/m2=240
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|thrust/weight=2.08
|more performance=
}}
Swept parm
{{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |span m=20 }}
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{{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |span m=20 |swept m=12 }}
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{{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |upper span m=15 |lower span m=20 }}
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{{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |upper span m=15 |lower span m=20 |swept m=12 }}
ref dump
{{reflist}}