Difference between revisions of "User:Jlmr"
From Kerbal Space Program Wiki
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m (→Template:Stats Table Jet Engines: -thumbnails;) |
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*Specific impulse at sea level on Kerbin is is calculated by the following equation. | *Specific impulse at sea level on Kerbin is is calculated by the following equation. | ||
− | ==Justification for t and kN (or 1000's kg and 1000's of N)== | + | ==Justification for t and kN (or 1000's kg and 1000's of N)== |
*An official NIST/SI publication: http://physics.nist.gov/Pubs/SP330/sp330.pdf states that kilonewton (kN) is a valid SI unit to represent 1000 N and ton (t), while historically a non-SI unit, has been accepted for use in the SI system by [[w:CIPM|CIPM]] as a valid unit to represent 1000 kg for just over a century. | *An official NIST/SI publication: http://physics.nist.gov/Pubs/SP330/sp330.pdf states that kilonewton (kN) is a valid SI unit to represent 1000 N and ton (t), while historically a non-SI unit, has been accepted for use in the SI system by [[w:CIPM|CIPM]] as a valid unit to represent 1000 kg for just over a century. | ||
Line 34: | Line 34: | ||
**If measured in metric tons, a "9 t" (9,000 kg) Rockomax X200-16 Fuel Tank under the same gravity, being about 0.67 m tall and 2 m in diameter, gives a volume of 2104.87 L, more than enough to hold the advertised 1600 L of fuel. Only a rocket engine with a thrust around 100 kN (100,000 N), could have any chance of lifting the 9 t (9,000 kg) fuel tank. | **If measured in metric tons, a "9 t" (9,000 kg) Rockomax X200-16 Fuel Tank under the same gravity, being about 0.67 m tall and 2 m in diameter, gives a volume of 2104.87 L, more than enough to hold the advertised 1600 L of fuel. Only a rocket engine with a thrust around 100 kN (100,000 N), could have any chance of lifting the 9 t (9,000 kg) fuel tank. | ||
**Similarly, a substance weighing only 8 kg with a volume of 1,600 L has a density of 5 kg/m3, only about three times greater than the density of gaseous oxygen, and would not make an efficient fuel. Whereas, a fuel weighing 8 t with a volume of 1,600 L has a density of 5000 kg/m3, closer to a realistic rocket fuel. | **Similarly, a substance weighing only 8 kg with a volume of 1,600 L has a density of 5 kg/m3, only about three times greater than the density of gaseous oxygen, and would not make an efficient fuel. Whereas, a fuel weighing 8 t with a volume of 1,600 L has a density of 5000 kg/m3, closer to a realistic rocket fuel. | ||
+ | |||
+ | =My "Sandbox"= | ||
+ | |||
+ | *'''Currently testing column widths and categories to standardize and future proof part tables. | ||
+ | ''' | ||
+ | ==Template:Stats Table Command Pods== | ||
+ | {| class="wikitable sortable" style=white-space:nowrap | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Image | ||
+ | |ru=Вид | ||
+ | |#default=Image | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="256px" | {{#switch:{{{1}}} | ||
+ | |=Part | ||
+ | |ru=Название | ||
+ | |#default=Part | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="80px" | {{#switch:{{{1}}} | ||
+ | |=Size | ||
+ | |ru=Размер | ||
+ | |#default=Size | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Cost ($) | ||
+ | |ru=Цена ($) | ||
+ | |#default=Cost ($) | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | |ru=[[wikipedia:ru:Масса|Масса]] [[wikipedia:ru:Тонна|(t)]] | ||
+ | |#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Drag_(physics)|Drag]] | ||
+ | |ru=[[wikipedia:ru:Лобовое_сопротивление|Лобовое сопротивление]] | ||
+ | |#default=[[w:Drag_(physics)|Drag]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Max Temp [[w:Kelvin|(K)]] | ||
+ | |ru=максимальная температура [[wikipedia:ru:Кельвин|(K)]] | ||
+ | |#default=Max Temp [[w:Kelvin|(K)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Tolerance | ||
+ | |ru=целостность конструкции | ||
+ | |#default=Tolerance | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Max [[SAS]] [[w:Torque|τ]] | ||
+ | |ru=Экипаж | ||
+ | |#default=Max [[SAS]] [[w:Torque|τ]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[Crew]] | ||
+ | |ru=Экипаж | ||
+ | |#default=[[Crew]] | ||
+ | }} | ||
+ | |||
+ | |- | ||
+ | | [[Image:MK1COCKPIT.png|60x60px|]] | ||
+ | | [[Mk1 Cockpit]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 1800 | ||
+ | | 1.25 | ||
+ | | 0.1 | ||
+ | | 3400 | ||
+ | | 45 | ||
+ | | 5 | ||
+ | | 1 | ||
+ | |- | ||
+ | | [[Image:Mk2cockpit.png|60x60px|]] | ||
+ | | [[Mk2 Cockpit]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 1600 | ||
+ | | 1 | ||
+ | | 0.08 | ||
+ | | 3400 | ||
+ | | 40 | ||
+ | | 5 | ||
+ | | 1 | ||
+ | |- | ||
+ | | [[Image:Mk3cockpit.png|60x60px|]] | ||
+ | | [[Mk3 Cockpit]] | ||
+ | | Mk3 | ||
+ | | 1600 | ||
+ | | 1 | ||
+ | | 0.2 | ||
+ | | 3400 | ||
+ | | 50 | ||
+ | | 5 | ||
+ | | 3 | ||
+ | |- | ||
+ | | [[Image:Command Pod Mk1.png|60x60px|]] | ||
+ | | [[Command Pod Mk1]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 600 | ||
+ | | 0.8 | ||
+ | | 0.2 | ||
+ | | 3400 | ||
+ | | 14 | ||
+ | | 5 | ||
+ | | 1 | ||
+ | |||
+ | |- | ||
+ | | [[Image:Mk1-2commandpod.png|60x60px|]] | ||
+ | | [[Mk1-2 Command Pod]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Large | ||
+ | |ru=Большое | ||
+ | |#default=Large | ||
+ | }} | ||
+ | | 1800 | ||
+ | | 4 | ||
+ | | 0.2 | ||
+ | | 3400 | ||
+ | | 45 | ||
+ | | 5 | ||
+ | | 3 | ||
+ | |} | ||
+ | |||
+ | ==Template:Stats Table Liquid Fuel Engines== | ||
+ | {| class="wikitable sortable" style=white-space:nowrap | ||
+ | |- | ||
+ | !colspan=10 style="background: #F9F9F9"| | ||
+ | !colspan=2|{{#switch:{{{1}}} | ||
+ | |=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]] | ||
+ | |ru=[[wikipedia:ru:Ракетное_топливо|топливо]] [[wikipedia:ru:Расходомер|(L/s)]] | ||
+ | |#default=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]] | ||
+ | }} | ||
+ | |||
+ | !colspan=2|{{#switch:{{{1}}} | ||
+ | |=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
+ | |ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]] | ||
+ | |#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
+ | }} | ||
+ | |||
+ | !colspan=1|{{#switch:{{{1}}} | ||
+ | |=[[w:Thrust_Vectoring|TVC]] | ||
+ | |ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]] | ||
+ | |#default=[[w:Thrust_Vectoring|TVC]] | ||
+ | }} | ||
+ | |- | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Image | ||
+ | |ru=Вид | ||
+ | |#default=Image | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="256px" | {{#switch:{{{1}}} | ||
+ | |=Part | ||
+ | |ru=Название | ||
+ | |#default=Part | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="80px" | {{#switch:{{{1}}} | ||
+ | |=Size | ||
+ | |ru=Размер | ||
+ | |#default=Size | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Cost ($) | ||
+ | |ru=Цена ($) | ||
+ | |#default=Cost ($) | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | |ru=[[wikipedia:ru:Масса|Масса]] [[wikipedia:ru:Тонна|(t)]] | ||
+ | |#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Drag_(physics)|Drag]] | ||
+ | |ru=[[wikipedia:ru:Лобовое_сопротивление|Лобовое сопротивление]] | ||
+ | |#default=[[w:Drag_(physics)|Drag]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Max Temp [[w:Kelvin|(K)]] | ||
+ | |ru=максимальная температура [[wikipedia:ru:Кельвин|(K)]] | ||
+ | |#default=Max Temp [[w:Kelvin|(K)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Tolerance | ||
+ | |ru=целостность конструкции | ||
+ | |#default=Tolerance | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Thrust [[w:Newton_(unit)|(kN)]] | ||
+ | |ru=Тяга [[wikipedia:ru:Ньютон_(единица_измерения)|(кН)]] | ||
+ | |#default=Thrust [[w:Newton_(unit)|(kN)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
+ | |ru=[[wikipedia:ru:Тяговооружённость|Тяговооружённость]] | ||
+ | |#default=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Atmosphere_(unit)|atm]] | ||
+ | |ru=[[wikipedia:ru:Атмосфера_(единица_измерения)|атм]] | ||
+ | |#default=[[w:Atmosphere_(unit)|atm]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Vacuum|vac]] | ||
+ | |ru=[[wikipedia:ru:Вакуум|вак]] | ||
+ | |#default=[[w:Vacuum|vac]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Atmosphere_(unit)|atm]] | ||
+ | |ru=[[wikipedia:ru:Атмосфера_(единица_измерения)|атм]] | ||
+ | |#default=[[w:Atmosphere_(unit)|atm]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Vacuum|vac]] | ||
+ | |ru=[[wikipedia:ru:Вакуум|вак]] | ||
+ | |#default=[[w:Vacuum|vac]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]] | ||
+ | |ru=[[wikipedia:ru:Карданов_подвес|Карданов подвес]] [[wikipedia:ru:Градус_(геометрия)|(°)]] | ||
+ | |#default=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]] | ||
+ | }} | ||
+ | |||
+ | |- | ||
+ | | [[File:Mark 55 Radial mount engine.png|60x60px|]] | ||
+ | | [[Rockomax Mark 55 Radial Mount Liquid Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Radial Mounted | ||
+ | |ru=Боковое | ||
+ | |#default=Radial Mounted | ||
+ | }} | ||
+ | | 850 | ||
+ | | 1.5 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 120 | ||
+ | | 8.2 | ||
+ | | 8.7 | ||
+ | | 7.4 | ||
+ | | 280 | ||
+ | | 330 | ||
+ | | 1.0 | ||
+ | |- | ||
+ | | [[File:LV-T30 Liquid Fuel Engine recent.png|60x60px|]] | ||
+ | | [[LV-T30 Liquid Fuel Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 850 | ||
+ | | 1.25 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 215 | ||
+ | | 17.5 | ||
+ | | 13.7 | ||
+ | | 11.8 | ||
+ | | 320 | ||
+ | | 370 | ||
+ | | - | ||
+ | |- | ||
+ | | [[File:LV-T45 LFE.png|60x60px|]] | ||
+ | | [[LV-T45 Liquid Fuel Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 950 | ||
+ | | 1.5 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 200 | ||
+ | | 13.6 | ||
+ | | 12.7 | ||
+ | | 11.0 | ||
+ | | 320 | ||
+ | | 370 | ||
+ | | 1.0 | ||
+ | |- | ||
+ | | [[File:LV-T909 LFE.png|60x60px|]] | ||
+ | | [[LV-909 Liquid Fuel Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 750 | ||
+ | | 0.5 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 50 | ||
+ | | 10.2 | ||
+ | | 3.4 | ||
+ | | 2.6 | ||
+ | | 300 | ||
+ | | 390 | ||
+ | | 0.5 | ||
+ | |- | ||
+ | | [[File:ToroidalAerospikeRocket.png|60x60px|]] | ||
+ | | [[Toroidal Aerospike Rocket]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 850 | ||
+ | | 1 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 20 | ||
+ | | 250 | ||
+ | | 25.5 | ||
+ | | 13.1 | ||
+ | | 13.1 | ||
+ | | 390 | ||
+ | | 390 | ||
+ | | - | ||
+ | |- | ||
+ | | [[File:RockomaxPoodle.png|60x60px|]] | ||
+ | | [[Rockomax "Poodle" Liquid Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Large | ||
+ | |ru=Большое | ||
+ | |#default=Large | ||
+ | }} | ||
+ | | 600 | ||
+ | | 2.5 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 220 | ||
+ | | 9.0 | ||
+ | | 16.6 | ||
+ | | 11.5 | ||
+ | | 270 | ||
+ | | 390 | ||
+ | | 2.5 | ||
+ | |- | ||
+ | | [[File:Rockomax Mainsail transparent.png|60x60px|]] | ||
+ | | [[Rockomax "Mainsail" Liquid Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Large | ||
+ | |ru=Большое | ||
+ | |#default=Large | ||
+ | }} | ||
+ | | 850 | ||
+ | | 6 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 1500 | ||
+ | | 25.5 | ||
+ | | 109.3 | ||
+ | | 92.7 | ||
+ | | 280 | ||
+ | | 330 | ||
+ | | 1.0 | ||
+ | |- | ||
+ | | [[File:LV-N Atomic.png|60x60px|]] | ||
+ | | [[LV-N Atomic Rocket Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 1700 | ||
+ | | 2.25 | ||
+ | | 0.2 | ||
+ | | 4000 | ||
+ | | 12 | ||
+ | | 60 | ||
+ | | 2.7 | ||
+ | | 5.5 | ||
+ | | 1.5 | ||
+ | | 220 | ||
+ | | 800 | ||
+ | | 1.0 | ||
+ | |- | ||
+ | |} | ||
+ | |||
+ | ==Template:Stats Table Solid Fuel Boosters== | ||
+ | {| class="wikitable sortable" style=white-space:nowrap | ||
+ | |- | ||
+ | !colspan=4| {{#switch:{{{1}}} | ||
+ | |=''Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron 1 is 31831 kg/m3)'' | ||
+ | |ru=''Плотность твердого топлива 1273-1910 кг/м3'' | ||
+ | |#default=''Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron 1 fuel density is 31831 kg/m3)'' | ||
+ | }} | ||
+ | !colspan=2| {{#switch:{{{1}}} | ||
+ | |=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | |ru=[[wikipedia:ru:Масса|Масса]] [[wikipedia:ru:Тонна|(t)]] | ||
+ | |#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | }} | ||
+ | !colspan=4| | ||
+ | !colspan=2| {{#switch:{{{1}}} | ||
+ | |=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
+ | |ru=[[wikipedia:ru:Тяговооружённость|Тяговооружённость]] | ||
+ | |#default=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
+ | }} | ||
+ | !colspan=2| | ||
+ | |- | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Image | ||
+ | |ru=Вид | ||
+ | |#default=Image | ||
+ | }} | ||
+ | ! scope="col" width="256px" | {{#switch:{{{1}}} | ||
+ | |=Part | ||
+ | |ru=Название | ||
+ | |#default=Part | ||
+ | }} | ||
+ | ! scope="col" width="80px" | {{#switch:{{{1}}} | ||
+ | |=Size | ||
+ | |ru=Размер | ||
+ | |#default=Size | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Cost ($) | ||
+ | |ru=Цена ($) | ||
+ | |#default=Cost ($) | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Full | ||
+ | |ru=Полный | ||
+ | |#default=Full | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Empty | ||
+ | |ru=Пустой | ||
+ | |#default=Empty | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Drag_(physics)|Drag]] | ||
+ | |ru=[[wikipedia:ru:Лобовое_сопротивление|Лобовое сопротивление]] | ||
+ | |#default=[[w:Drag_(physics)|Drag]] | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Max Temp [[w:Kelvin|(K)]] | ||
+ | |ru=максимальная температура [[wikipedia:ru:Кельвин|(K)]] | ||
+ | |#default=Max Temp [[w:Kelvin|(K)]] | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Tolerance | ||
+ | |ru=целостность конструкции | ||
+ | |#default=Tolerance | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Thrust [[w:Newton_(unit)|(kN)]] | ||
+ | |ru=Тяга [[wikipedia:ru:Ньютон_(единица_измерения)|(кН)]] | ||
+ | |#default=Thrust [[w:Newton_(unit)|(kN)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Full | ||
+ | |ru=Полный | ||
+ | |#default=Full | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Empty | ||
+ | |ru=Пустой | ||
+ | |#default=Empty | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]] | ||
+ | |ru=[[wikipedia:ru:Твердотопливный_ракетный_двигатель|Время горения]] [[wikipedia:ru:Секунда|(с)]] | ||
+ | |#default=[[w:Solid-fuel_rocket|Burn]] [[w:Second|(s)]] | ||
+ | }} | ||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
+ | |ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]] | ||
+ | |#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
+ | }} | ||
+ | |- | ||
+ | | [[Image:RT-10.png|60x60px|]] | ||
+ | | [[RT-10 Solid Fuel Booster]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 450 | ||
+ | | 3.5 | ||
+ | | 0.5 | ||
+ | | 0.3 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 250 | ||
+ | | 7.3 | ||
+ | | 51.0 | ||
+ | | 25 | ||
+ | | 212 | ||
+ | |- | ||
+ | | [[Image:BACC_SFB.png|60x60px|]] | ||
+ | | [[Rockomax BACC Solid Fuel Booster]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 800 | ||
+ | | 6.75 | ||
+ | | 0.75 | ||
+ | | 0.3 | ||
+ | | 3900 | ||
+ | | 7 | ||
+ | | 550 | ||
+ | | 7.6 | ||
+ | | 68.0 | ||
+ | | 30 | ||
+ | | 280 | ||
+ | |- | ||
+ | | [[Image:Sepratron.png|60x60px|]] | ||
+ | | [[Sepratron I]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Radial Mounted | ||
+ | |ru=Боковое | ||
+ | |#default=Radial Mounted | ||
+ | }} | ||
+ | | 100 | ||
+ | | 0.15 | ||
+ | | 0.05 | ||
+ | | 0.3 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 20 | ||
+ | | 13.6 | ||
+ | | 40.8 | ||
+ | | 5 | ||
+ | | 102 | ||
+ | |} | ||
+ | |||
+ | ==Template:Stats Table Jet Engines== | ||
+ | {| class="wikitable sortable" style=white-space:nowrap | ||
+ | |- | ||
+ | !colspan=11| | ||
+ | !colspan=1|{{#switch:{{{1}}} | ||
+ | |=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
+ | |ru=[[wikipedia:ru:Удельный_импульс|Удельный импульс]] [[wikipedia:ru:Секунда|(с)]] | ||
+ | |#default=[[w:Specific_impulse|Isp]] [[w:Second|(s)]] | ||
+ | }} | ||
+ | !colspan=1|{{#switch:{{{1}}} | ||
+ | |=[[w:Thrust_Vectoring|TVC]] | ||
+ | |ru=[[wikipedia:ru:Управление_вектором_тяги|УВТ]] | ||
+ | |#default=[[w:Thrust_Vectoring|TVC]] | ||
+ | }} | ||
+ | !colspan=3|{{#switch:{{{1}}} | ||
+ | |=Intake | ||
+ | |ru=впускного | ||
+ | |#default=Intake | ||
+ | }} | ||
+ | |- | ||
+ | ! {{#switch:{{{1}}} | ||
+ | |=Image | ||
+ | |ru=Вид | ||
+ | |#default=Image | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="256px" | {{#switch:{{{1}}} | ||
+ | |=Part | ||
+ | |ru=Название | ||
+ | |#default=Part | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="80px" | {{#switch:{{{1}}} | ||
+ | |=Size | ||
+ | |ru=Размер | ||
+ | |#default=Size | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Cost ($) | ||
+ | |ru=Цена ($) | ||
+ | |#default=Cost ($) | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | |ru=[[wikipedia:ru:Масса|Масса]] [[wikipedia:ru:Тонна|(t)]] | ||
+ | |#default=[[w:Mass|Mass]] [[w:Metric_Ton|(t)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Drag_(physics)|Drag]] | ||
+ | |ru=[[wikipedia:ru:Лобовое_сопротивление|Лобовое сопротивление]] | ||
+ | |#default=[[w:Drag_(physics)|Drag]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Max Temp [[w:Kelvin|(K)]] | ||
+ | |ru=максимальная температура [[wikipedia:ru:Кельвин|(K)]] | ||
+ | |#default=Max Temp [[w:Kelvin|(K)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Tolerance | ||
+ | |ru=целостность конструкции | ||
+ | |#default=Tolerance | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Thrust [[w:Newton_(unit)|(kN)]] | ||
+ | |ru=Тяга [[wikipedia:ru:Ньютон_(единица_измерения)|(кН)]] | ||
+ | |#default=Thrust [[w:Newton_(unit)|(kN)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
+ | |ru=[[wikipedia:ru:Тяговооружённость|Тяговооружённость]] | ||
+ | |#default=[[w:Thrust-to-weight_ratio|T/W ratio]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]] | ||
+ | |ru=[[wikipedia:ru:Ракетное_топливо|топливо]] [[wikipedia:ru:Расходомер|(L/s)]] | ||
+ | |#default=[[w:Rocket_propellant|Fuel]] [[w:Flow_measurement|(L/s)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Atmosphere_(unit)|atm]] | ||
+ | |ru=[[wikipedia:ru:Атмосфера_(единица_измерения)|атм]] | ||
+ | |#default=[[w:Atmosphere_(unit)|atm]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]] | ||
+ | |ru=[[wikipedia:ru:Карданов_подвес|Карданов подвес]] [[wikipedia:ru:Градус_(геометрия)|(°)]] | ||
+ | |#default=[[w:Gimbal|Gimbal]] [[w:Degree_(angle)|(°)]] | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Airflow | ||
+ | |ru=воздушный поток | ||
+ | |#default=Airflow | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Size | ||
+ | |ru=Размер | ||
+ | |#default=Size | ||
+ | }} | ||
+ | |||
+ | ! scope="col" width="60px" | {{#switch:{{{1}}} | ||
+ | |=Power | ||
+ | |ru=Впускной | ||
+ | |#default=Power | ||
+ | }} | ||
+ | |||
+ | |- | ||
+ | | [[Image:Basicjetengine.png|60x60px|]] | ||
+ | | [[Basic Jet Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 950 | ||
+ | | 1 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 100 | ||
+ | | 10.2 | ||
+ | | 0.3 | ||
+ | | 1456 <sub>stall</sub> - 7282 <sub>max</sub> | ||
+ | | 2.5 | ||
+ | | 200 | ||
+ | | 1.1 | ||
+ | | 125 | ||
+ | |- | ||
+ | | [[Image:Turbojetengine.png|60x60px|]] | ||
+ | | [[TurboJet Engine]] | ||
+ | | {{#switch:{{{1}}} | ||
+ | |=Small | ||
+ | |ru=Маленькое | ||
+ | |#default=Small | ||
+ | }} | ||
+ | | 950 | ||
+ | | 1.2 | ||
+ | | 0.2 | ||
+ | | 3600 | ||
+ | | 7 | ||
+ | | 150 | ||
+ | | 12.7 | ||
+ | | 0.4 | ||
+ | | 546 <sub>stall</sub> - 8192 <sub>max</sub> | ||
+ | | 2.5 | ||
+ | | 60 | ||
+ | | 1.0 | ||
+ | | 200 | ||
+ | |- | ||
+ | |} |
Latest revision as of 10:02, 24 April 2014
KSP is just what I have been looking for! A creative space simulator! Now if the team at Squad would just add little things like, ships, air balloons, zeplins, bombs, guns, missiles, subs, lasers, ground combat, animals, city/nation building, multiplayer, space colonies, space docks, space construction yards, asteroid mining, resources/economy... Hey, I can hope right? =)
Kerbals at War = OMG!!! *drools*
Contents
My stuff
Units of measure
- While units of mass and thrust are not specifically labeled in-game, a bit of logic can quickly determine that thrust is measured in kilonewtons (kN) and mass in metric tons (t). For example, if measured in kilograms(kg), a "9 kg" Rockomax X200-16 Fuel Tank on Kerbin, having a surface gravity of 9.81 m/s2, would be roughly the size of a 48 oz coffee tin and only hold about 1.5 L of fuel. If measured in metric tons, a 9 t Rockomax X200-16 Fuel Tank under the same gravity would be about 0.67 m tall and 2 m in diameter, easily capable of holding the advertised 1600 L of fuel. Only a rocket engine with a thrust around 100 kN could have any chance to lift a 9 t fuel tank.
- Thrust to weight ratio at sea level on Kerbin is calculated by the following equation, which applies only to liquid or solid fuel rocket engines, jet engines use a complicated formula on a vehicle to vehicle basis.
where:
- is the thrust is the thrust obtained from the engine, in kilonewtons.
- is the weight of the engine at sea level on Kerbin's surface.
- is the mass of the engine in metric tons (t).
- is the acceleration at sea level on Kerbin's surface, in m/s² (≈9.807 m/s²).
- Specific impulse at sea level on Kerbin is is calculated by the following equation.
Justification for t and kN (or 1000's kg and 1000's of N)
- An official NIST/SI publication: http://physics.nist.gov/Pubs/SP330/sp330.pdf states that kilonewton (kN) is a valid SI unit to represent 1000 N and ton (t), while historically a non-SI unit, has been accepted for use in the SI system by CIPM as a valid unit to represent 1000 kg for just over a century.
- We already know that the game uses SI units. These are specifically labeled: meters for units of distance, meters/sec for acceleration, liters for fuel volume, and liters/sec for fuel consumption.
- We know that the Mk1-2 Command Pod weighs 4 "units" from the in-game description. The command pod is roughly 2 m in height and 2 m in diameter. Calculating it's total volume gives us about 2.09 m3. Let's assume the capsule has 0.05 m (2 in) thick walls and subtract the interior void to get only the volume of the capsule walls. This gives us a volume of 1.80 m3.
- Knowing the volume of the walls, we can calculate the density of the material making up the capsule, taking the 4 in-game units to mean kg, this comes out to be about 13.79 kg/m3. Unfortunately, is about 72.29 times less dense than water at room temperature and closer in density to most gasses! Perhaps Kerbals have discovered a super strong gas-like substance to make spaceships from? =)
- However, if we take the 4 in-game units to mean metric tons, we get a density of around 13793.10 kg/m3, well within the range of the density of real building materials.
- The wikipage on Kerbin states it has a surface gravity of 9.81 m/s2, roughly that of Earth.
- Given this we can calculate the following. If measured in kilograms(kg), a "9 kg" Rockomax X200-16 Fuel Tank on Kerbin, having a surface gravity of 9.81 m/s2, would be roughly the size of a 48 oz coffee tin and only hold about 1.5 L of fuel. Unfortunately for our intrepid Kerbals, 1.5 L of fuel would not provide enough energy to lift a 9 kg payload through 75,000 m of atmosphere, much less a few hundred meters.
- If measured in metric tons, a "9 t" (9,000 kg) Rockomax X200-16 Fuel Tank under the same gravity, being about 0.67 m tall and 2 m in diameter, gives a volume of 2104.87 L, more than enough to hold the advertised 1600 L of fuel. Only a rocket engine with a thrust around 100 kN (100,000 N), could have any chance of lifting the 9 t (9,000 kg) fuel tank.
- Similarly, a substance weighing only 8 kg with a volume of 1,600 L has a density of 5 kg/m3, only about three times greater than the density of gaseous oxygen, and would not make an efficient fuel. Whereas, a fuel weighing 8 t with a volume of 1,600 L has a density of 5000 kg/m3, closer to a realistic rocket fuel.
My "Sandbox"
- Currently testing column widths and categories to standardize and future proof part tables.
Template:Stats Table Command Pods
Image | Part | Size | Cost ($) | Mass (t) | Drag | Max Temp (K) | Tolerance | Max SAS τ | Crew |
---|---|---|---|---|---|---|---|---|---|
Mk1 Cockpit | Small | 1800 | 1.25 | 0.1 | 3400 | 45 | 5 | 1 | |
Mk2 Cockpit | Small | 1600 | 1 | 0.08 | 3400 | 40 | 5 | 1 | |
Mk3 Cockpit | Mk3 | 1600 | 1 | 0.2 | 3400 | 50 | 5 | 3 | |
Command Pod Mk1 | Small | 600 | 0.8 | 0.2 | 3400 | 14 | 5 | 1 | |
Mk1-2 Command Pod | Large | 1800 | 4 | 0.2 | 3400 | 45 | 5 | 3 |
Template:Stats Table Liquid Fuel Engines
Fuel (L/s) | Isp (s) | TVC | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Image | Part | Size | Cost ($) | Mass (t) | Drag | Max Temp (K) | Tolerance | Thrust (kN) | T/W ratio | atm | vac | atm | vac | Gimbal (°) |
Rockomax Mark 55 Radial Mount Liquid Engine | Radial Mounted | 850 | 1.5 | 0.2 | 3600 | 7 | 120 | 8.2 | 8.7 | 7.4 | 280 | 330 | 1.0 | |
LV-T30 Liquid Fuel Engine | Small | 850 | 1.25 | 0.2 | 3600 | 7 | 215 | 17.5 | 13.7 | 11.8 | 320 | 370 | - | |
LV-T45 Liquid Fuel Engine | Small | 950 | 1.5 | 0.2 | 3600 | 7 | 200 | 13.6 | 12.7 | 11.0 | 320 | 370 | 1.0 | |
LV-909 Liquid Fuel Engine | Small | 750 | 0.5 | 0.2 | 3600 | 7 | 50 | 10.2 | 3.4 | 2.6 | 300 | 390 | 0.5 | |
Toroidal Aerospike Rocket | Small | 850 | 1 | 0.2 | 3600 | 20 | 250 | 25.5 | 13.1 | 13.1 | 390 | 390 | - | |
Rockomax "Poodle" Liquid Engine | Large | 600 | 2.5 | 0.2 | 3600 | 7 | 220 | 9.0 | 16.6 | 11.5 | 270 | 390 | 2.5 | |
Rockomax "Mainsail" Liquid Engine | Large | 850 | 6 | 0.2 | 3600 | 7 | 1500 | 25.5 | 109.3 | 92.7 | 280 | 330 | 1.0 | |
LV-N Atomic Rocket Engine | Small | 1700 | 2.25 | 0.2 | 4000 | 12 | 60 | 2.7 | 5.5 | 1.5 | 220 | 800 | 1.0 |
Template:Stats Table Solid Fuel Boosters
Solid Fuel Density is 1273-1910 kg/m3 - (Sepratron 1 fuel density is 31831 kg/m3) | Mass (t) | T/W ratio | |||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Image | Part | Size | Cost ($) | Full | Empty | Drag | Max Temp (K) | Tolerance | Thrust (kN) | Full | Empty | Burn (s) | Isp (s) |
RT-10 Solid Fuel Booster | Small | 450 | 3.5 | 0.5 | 0.3 | 3600 | 7 | 250 | 7.3 | 51.0 | 25 | 212 | |
Rockomax BACC Solid Fuel Booster | Small | 800 | 6.75 | 0.75 | 0.3 | 3900 | 7 | 550 | 7.6 | 68.0 | 30 | 280 | |
Sepratron I | Radial Mounted | 100 | 0.15 | 0.05 | 0.3 | 3600 | 7 | 20 | 13.6 | 40.8 | 5 | 102 |
Template:Stats Table Jet Engines
Isp (s) | TVC | Intake | |||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Image | Part | Size | Cost ($) | Mass (t) | Drag | Max Temp (K) | Tolerance | Thrust (kN) | T/W ratio | Fuel (L/s) | atm | Gimbal (°) | Airflow | Size | Power |
Basic Jet Engine | Small | 950 | 1 | 0.2 | 3600 | 7 | 100 | 10.2 | 0.3 | 1456 stall - 7282 max | 2.5 | 200 | 1.1 | 125 | |
TurboJet Engine | Small | 950 | 1.2 | 0.2 | 3600 | 7 | 150 | 12.7 | 0.4 | 546 stall - 8192 max | 2.5 | 60 | 1.0 | 200 |