قالب:جدول مرحلة صاروخ

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 Usage

{{{name}}}

[[File:{{{image}}}|{{{image_size}}}|alt={{{alt}}}]] {{{caption}}}
الصانع	{{{manufacturer}}}
بلد المنشأ	{{{country-origin}}}
تـُستخدَم في	{{{rockets}}}
السمات العامة
الارتفاع	{{{height}}} ({{{alt-height}}})
القطر	{{{diameter}}} ({{{alt-diameter}}})
الطول	{{{length}}}
العرض	{{{width}}}
الكتلة القائمة	{{{mass}}} ({{{alt-mass}}})
كتلة الوقود	{{{propmass}}} ({{{alt-propmass}}})
الكتلة الفارغة	{{{empty}}}
المراحل	{{{stages}}}
المراحل المرافقة
العائلة	{{{family}}}
مشتق من	{{{derived_from}}}
المشتقات	{{{derivatives}}}
القرائن	{{{comparable}}}
تاريخ الإطلاق
الوضع	{{{status}}}
إجمالي مرات الإطلاق	{{{launches}}}
مرات النجاح (المرحلة فقط)	{{{success}}}
الفشل	{{{fail}}}
فشل مرحلة سفلى	{{{noburn}}}
غيره	{{{other_outcome}}}
أول تحليق	{{{first}}}
آخر تحليق	{{{last}}}
تاريخ الإطلاق	{{{only}}}
{{{stagedata}}}
{{{name}}}
المحركات	{{{engines}}}
الدفع	{{{thrust}}}
الاندفاع النوعي	{{{SI}}}
وقت الاحتراق	{{{time}}}
الوقود	{{{fuel}}}

All parameters except engines, thrust, and fuel are optional.

{{Infobox rocket stage
<!-- Image -->
| image         = <!--image filename (omit "Image:" prefix)-->
| caption       = <!--image caption-->
<!-- Basic information -->
| name          = <!--becomes infobox title-->
| manufacturer  = <!--stage manufacturer-->
| country       = <!--country of origin, do not use flag-->
| rockets       = <!--vehicle(s) stage was used on-->
<!-- General characteristics -->
| height        = <!--height in meters, use {{convert}}-->
| diameter      = <!--diameter in meters, use {{convert}}-->
| mass          = <!--gross mass in kilograms, use {{convert}}-->
| propmass      = <!--propellant mass in kilograms, use {{convert}}-->
| empty         = <!--dry mass in kilograms, use {{convert}}-->
<!-- Associated Stages -->
| family        = <!--if a member of a family of stages-->
| derived_from  = <!--if derived from another stage or stages-->
| derivatives   = <!--if derivative stages-->
| comparable    = <!--if any similar, unrelated stage-->
<!-- Launch history -->
| status        = <!--active, retired, under development, cancelled, etc-->
| launches      = <!--total launches to date-->
| success       = <!--number of times stage has operated successfully-->
| fail          = <!--number of times stage itself has failed-->
| noburn        = <!--lower stage failed-->
| other_outcome = <!--other-->
| first         = <!--date of first flight-->
| last          = <!--date of last flight-->
| only          = <!--date of launch if stage flew only once-->
<!--Engine details (optional)-->
| stagedata     = <!--insert one of the following templates for each engine types:-->
{{Infobox rocket/stage
| name          =
| engines       = <!--number of engines used on the rocket stage-->
| solid         = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
| thrust        = <!--thrust provided by a single engine in kN, use {{cvt|THRUST|kN}}-->
| SI            = <!--specific impulse of an individual engine, in seconds, use {{convert|ISP_IN_SECONDS|isp}}-->
| burntime      = <!--burn time-->
| fuel          = <!--fuel used in engine-->
}}
}}

 Obsolete (legacy) parameters

These parameters are supported by the template to allow it to display properly on articles that have not yet been converted to the new format. They should not be introduced into new articles/transclusions.

| alt-height    = <!--height in feet-->
| alt-diameter  = <!--diameter in feet-->
| alt-mass      = <!--gross mass in pounds-->
| alt-propmass  = <!--propellant mass in pounds-->
| alt-thrust    = <!--thrust in lbf-->
<!-- Engine details -->
| engines       = <!--number and type of engines used stage, required-->
| thrust        = <!--thrust provided by stage in kN, use {{convert}}, required-->
| SI            = <!--specific impulse of stage in s-->
| time          = <!--stage burn time in s -->
| fuel          = <!--propellant used in stage, required-->

 Example

S-II

ملف:Ap6-MSFC-6758331.jpg The Apollo 6 S-II stage during stacking operations in the VAB
الصانع	North American
بلد المنشأ	USA
تـُستخدَم في	Saturn V (stage 2) Saturn INT-21 (stage 2)
السمات العامة
الارتفاع	24.9 m (82 ft)
القطر	10 m (33 ft)
الكتلة القائمة	480,000 kg (1,058,000 lb)
كتلة الوقود	443,000 kg (977,000 lb)
الكتلة الفارغة	36,200 kg (79,700 lb)
تاريخ الإطلاق
الوضع	Retired
إجمالي مرات الإطلاق	13
مرات النجاح (المرحلة فقط)	12
غيره	Partial failure (Apollo 6)
أول تحليق	November 9, 1967 (AS-501) Apollo 4
آخر تحليق	May 14, 1973 (AS-513) Skylab 1
Saturn V S-II
المحركات	5 Rocketdyne J-2
الدفع	4,400 kN (1,000,000 lbf)
الاندفاع النوعي	421 seconds (4.13 km/s)
وقت الاحتراق	367 s
الوقود	LOX/LH2

{{Infobox rocket stage
| image         = ap6-MSFC-6758331.jpg
| caption       = The [[Apollo 6]] S-II stage during stacking operations in the [[Vehicle Assembly Building|VAB]]
| name          = S-II
| manufacturer  = [[North American Aviation|North American]]
| country       = USA
| rockets       = [[Saturn V]] (stage 2)<br>[[Saturn INT-21]] (stage 2)
| height        = {{convert|24.9|m|abbr=on}}
| diameter      = {{convert|10|m|abbr=on}}
| mass          = {{convert|1058000|lbs|abbr=on|order=flip}}
| propmass      = {{convert|977000|lbs|abbr=on|order=flip}}
| empty         = {{convert|79700|lbs|abbr=on|order=flip}}
| status        = Retired
| launches      = 13
| success       = 12
| other_outcome = Partial failure ([[Apollo 6]])
| first         = November 9, 1967 (AS-501) [[Apollo 4]]
| last          = May 14, 1973 (AS-513) [[Skylab 1]]
| stagedata     =
{{Infobox rocket/stage
| name          = Saturn V S-II
| engines       = 5 [[Rocketdyne J-2]]
| thrust        = {{convert|1000000|lbf|kN|abbr=on|order=flip}}
| SI            = {{convert|421|isp}}
| burntime      = 367 s
| fuel          = [[أكسجين سائل|LOX]]/[[هيدروجين سائل|LH<sub>2</sub>]]
}}
}}

 Tracking categories

• Category:Pages using infobox rocket stage with unknown parameters (0)
• Category:Rocketry articles with outdated infoboxes (21)

 See also