
Na první pohled úplně obyčejný Clarion...

...na druhý ovšem je vidět, že jde o nový kousek Clarion-S alias "Shorty"

Je určený k vynášení nákladů s vlastním pohonem, jako je kupříkladu tento lunární lander...

Bez komentáře...

Moderátor: jarl
Kód: Vybrat vše
// 100 "fuel unit" = F45 + O55; = M 93,75; = Xe 4250
// 100 "fuel unit" = 0.5 m^3
// 200 "fuel unit" = 1 m^3
// battery (store 1000 ElectricCharge) mass 0,05t; volume 40 "fuel unit" , price 1000
// OX-STAT solar panel (for CM/SM/EM modules): mass 0,005; price 50 (per one 100% panel) output = (intiger of) number of panels x 0,75 x 0,2
// RTG generator (one module) mass 0.15, volume 10 fuel unit, price 3500 output 1,5 electric charge per sec, need 1 build-in CoolingPanelA1 per 1 unit in CM/SM/EM model)
// module "Reaction Wheel1": mass 0.01 volume 1 fuel unit, price 10 energy consumption 0,005EC (per 1 unit of torque)
// module "Reaction Wheel2" Mini: mass 0.015 volume 0.25 fuel unit price 25 energy consumption 0,01EC (per 1 unit of torque) (miniaturized for small volume container)
// module SAS1: mass 0,05 volume 40 fuel unit price 500
// module SAS2 Mini: mass 0,025 volume 10 fuel unit price 1250 K (miniturized, for small volume container)
// module Command1: mass 0,05 volume 40 fuel unit price 500 K energy consumption 0,05EC
// module Command2Mini: mass 0,025 colume 10 fuel unit, price 1250 K, energy consumption 0,05EC (miniturized, for small volume container)
// penalty (for CM/SM/EM modules): price +250K for +1 fuel unit over limit, mass +0,05 for 1 fuel unit over limit, max penalty 5 fuel unit, max 2% of max. fuel unit
// Engine
// total price (BASE + alternator + gimball) + sidemount + aerodynamic cover
// multimode engine count as two engine Mode1 (base+alternator+gimbal) + Mode2 (base+alternator+gimbal) + sidemount + aerodynamic cover
// BASE: ((thrust x ((Isp(vac)+Isp(sl)/2) / ((mass in ton)x100 x base diameter in meter)) x (tolerance/10)
// nonstandard fuel BASE x1,5 for monoprop; x2,5 for cryogenic; x5 for nuclear; x0,1 for airbreathing
// alternator output x50
// gimball thrust x gimballRange/2
// side mount BASE x 0.125
// aerodynamic cover BASE x base diameter in meter x 0,25
// Tanks
// dimension, area, price and mass
// calculated area: Pi*D^2 + Pi*D*H
_________ (Pi*D^2)/4
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Pi*D*H |=========| 2*(Pi*D^2)/4
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|_________| (Pi*D^2)/4
_______________________________
Pi*D*H + 4*(Pi*D^2)/4 = Pi*D*H + Pi*D^2
// D=2,5m H=15m => A=137,5m2
// mass = 0,015 t/m^2 for liquid fuel, oxidizer
// mass = 0,020 t/m^2 for momopropellant and agresive liquids
// mass = 0,025 t/m^2 for for Xenon and other pressurized gases
// mass +25% for reinforced tanks (crashTolerance > 10 < 25)
// mass +25% for cryogenic tanks
// price = 40 per m2 for liquid fuel, oxidizer and other normal liquids (include liquificed gases)
// price = 100 per m2 for momopropellant and agresive liquids
// price = 200 per m2 for for Xenon and other pressurized gases
// price +25% for reinforced tanks (crashTolerance > 10 < 25)
// price +25% for cryogenic tanks