Oct 08, 2019 Cheat Sheets for Kerbal Space Program This is a collection of cheat sheets for the game Kerbal Space Program developed by SQUAD. The Delta-v maps are based on work by WAC and Kowgan on the Kerbal Space Program Forums as well as the Kerbal Space Program community on Reddit The font used is called Aller and can be downloaded on FontSquirrel. Credit for the center image: u/gmiezis from his high-res loading screen for KSP. If anyone is interested I can upload the.psd file so the action groups can be edited. Edit: wow thanks for all the support everyone. I will post the psd when I get home from work. And thanks for pointing out incorrect info. I will verify and fix once I have time.

1. How Do You Cheat A Craft Into Orbit? - Kerbal Space Program ...
2. Cached
3. Ksp Cheat Sheet
4. Cheat Sheet For Chemical Equilibrium

This is a list of the default key bindings of the standard game.Please note that PlayStation 4 and Xbox One bindings have not been included as of yet for either the Enhanced Edition or the original port! (the Enhanced Edition pause menu does have a list of controls)

Modifier key

Because KSP can run on different operating systems the modifier key (Mod) differs between them. In the table below, the default Mod key is mapped to the following keys (to use a different key, edit the entry in the'MODIFIER_KEY' section of the settings.cfg file):

• Windows: ⎇ Alt (e. g. ⎇ Alt+L)
• Mac OS: ⌥ Option (e. g. ⌥ Opt+L)
• Linux: KSP 1.1+: Right-Shift (e. g. Right-Shift+L) Don't confuse this with Left-Shift, which will fire your engines! KSP 1.0.5 and earlier uses a different key, which can cause issues in some window managers when playing in windowed mode. ^[1]

As an example, Mod+L locks the current stage. The key combinations in brackets show an example of the respective operating system's key combination: just swap Mod with the operating system's designated modifier.

Some keyboards also require to press a Fn key to access some special keys like F5. For example, Macs and some Linux devices such as ThinkPad, require Fn+F5.

Highlight legend

• - RCS
• - SAS
• - VAB/SPH
• - EVA
• - Docking

Key Bindings for English keyboard layout

External links

• As PDF – Controls of version 0.22.0 as one single paged PDF

• As XLSX – Controls of version 0.22.0 as Excel Spreadsheet

• As PDF – Controls of version 0.18.0 as one single paged PDF

• As PDF – Controls of version 1.2.2 as one single paged PDF

(Deze pagina wordt nog vertaald)Kerbal space program raketwetenschappers cheat sheet: Delta-v kaarten, formules en meer voor jou referentie, zodat je van hier naar daar en weer terug kan

• 1Wiskunde
  • 1.3Delta-v (Δv)
• 2Math examples

Wiskunde

Kracht/Gewicht Ratio (TWR)

→ See also: Thrust-to-weight ratio

Dit is de tweede wet van Newton. Als de ratio kleiner dan 1 is, zal het voertuig niet van de grond komen. Je moet wel rekening houden met de zwaartekracht van de lanceerplaats en de manier van lanceren: een vliegtuig zal eerder van de grond komen, omdat vliegtuigen gebruik maken van horizontale snelheid. Ook zal een raket een hogere TWR hebben op bijvoorbeeld Minmus, omdat daar een lagere aantrekkingskracht aanwezig is.

• ${\displaystyle F_T}$ Kracht van de motoren
• ${\displaystyle m}$ Totale massa van het object
• ${\displaystyle g}$ Lokale versnelling van de zwaartekracht (Oppervlaktezwaartekracht)

Gecombineerde specifieke stoot (I_sp)

How Do You Cheat A Craft Into Orbit? - Kerbal Space Program ...

→ See also: Specific impulse

Als de I_sp hetzelfde is voor alle motoren in een trap, dan is de I_sp gelijk aan die van een motor van hetzelfde soort. Als de I_sp verschillend is voor de motoren in een trap, gebruik je de volgende formule:

${\displaystyle I_{sp}=\frac{(F_1+F_2+\dots )}{\frac{F_1}{I_{sp1}}+\frac{F_2}{I_{sp2}}+\dots }}$

Delta-v (Δv)

Basis berekening

→ See also: Tutorial:Advanced Rocket Design

Basic calculation of a rocket's Δv. Use the atmospheric and vacuum thrust values for atmospheric and vacuum Δv, respectively.

• ${\displaystyle \mathrm{\Delta }v}$ Is de verandering van snelheid in m/s

Basis berekening voor een raket is de Δv. Gebruik de Atmosferische waarden voor in de Atmosfeer, en de vacuum waarden voor in de ruimte.

• ${\displaystyle M_{start}}$ Is de start massa van de raket ${\displaystyle M_{end}}$
• ${\displaystyle M_{end}}$ Is de massa van de raket zonder brandstof ${\displaystyle M_{start}}$
• ${\displaystyle I_{sp}}$ Is de specifieke stoot van de motoren in seconden.

Echte Δv van een stage die begint in de atmosfeer op het lanceerplatform en eindigt in de ruimte

Het berekenen van de Δv van een rakettrap kan een ander getal geven als de raket nog moet beginnen in de atmosfeer, bijvoorbeeld op het lanceerplatform. Δv_out is the hoeveelheid Δv die nodig is om de atmosfeer van een hemellichaam te verlaten, NIET om een baan te bereiken. Deze formule is handig om uit te vinden of de hoeveelheid Δv in de Transition stage genoeg is om van de atmosfeer in de ruimte te komen.

${\displaystyle \mathrm{\Delta }{v}_T=\frac{\mathrm{\Delta }{v}_{atm}-\mathrm{\Delta }{v}_{out}}{\mathrm{\Delta }{v}_{atm}}\cdot \mathrm{\Delta }{v}_{vac}+\mathrm{\Delta }{v}_{out}}$

Maps

Een fan made map die laat zien hoeveel Δv nodig is om naar een andere plek te gaan.

Total Δv values

Δv change values

Δv nomogram

Math examples

TWR

• Copy template:

TWR = F / (m * g) > 1

I_sp

Cached

1. When I_sp is the same for all engines in a stage, then the I_sp is equal to a single engine. So six 200 I_sp engines still yields only 200 I_sp.
2. When I_sp is different for engines in a single stage, then use the following equation:

• Equation:

${\displaystyle I_{sp}=\frac{(F_1+F_2+\dots )}{\frac{F_1}{I_{sp1}}+\frac{F_2}{I_{sp2}}+\dots }}$

• Simplified:

I_sp = ( F1 + F2 + ... ) / ( ( F1 / I_sp1 ) + ( F2 / I_sp2 ) + ... )

• Explained:

I_sp = ( Force of Thrust of 1st Engine + Force of Thrust of 2nd Engine...and so on... ) / ( ( Force of Thrust of 1st Engine / I_sp of 1st Engine ) + ( Force of Thrust of 2nd Engine / I_sp of 2nd Engine ) + ...and so on... )

• Example:

Two engines, one rated 200 newtons and 120 seconds I_sp ; another engine rated 50 newtons and 200 seconds I_sp.

Isp = (200 newtons + 50 newtons) / ( ( 200 newtons / 120 ) + ( 50 newtons / 200 ) = 130.89 seconds I_sp

Ksp Cheat Sheet

Δv

1. For atmospheric Δv value, use atmospheric thrust values.
2. For vacuum Δv value, use vacuum thrust values.
3. Use this equation to figure out the Δv per stage:

• Equation:

${\displaystyle \mathrm{\Delta }v=ln\left(\frac{M_{start}}{M_{dry}}\right)\cdot I_{sp}\cdot 9.81\frac{m}{s^2}}$

• Simplified:

Δv = ln ( Mstart / Mdry ) * I_sp * g

• Explained:

Δv = ln ( Starting Mass / Dry Mass ) X Isp X 9.81

• Example:

Cheat Sheet For Chemical Equilibrium

Single Stage Rocket that weighs 23 tons when full, 15 tons when fuel is emptied, and engine that outputs 120 seconds I_sp.

Δv = ln ( 23 Tons / 15 Tons ) × 120 seconds I_sp × 9.81m/s = Total Δv of 1803.2 m/s2

True Δv

1. How to calculate the Δv of a rocket stage that transitions from Kerbin atmosphere to vacuum.
2. Assumption: It takes approximately 1000 m/s2 of Δv to escape Kerbin's atmosphere before vacuum Δv values take over for the stage powering the transition.
3. Note: This equation is an guess, approximation, and is not 100% accurate. Per forum user stupid_chris who came up with the equation: 'The results will vary a bit depending on your TWR and such, but it should usually be pretty darn accurate.'

• Equation for Kerbin Atmospheric Escape:

${\displaystyle \mathrm{\Delta }{v}_T=\frac{\mathrm{\Delta }{v}_{atm}-\mathrm{\Delta }{v}_{out}\frac{m}{s^2}}{\mathrm{\Delta }{v}_{atm}}\cdot \mathrm{\Delta }{v}_{vac}+\mathrm{\Delta }{v}_{out}\frac{m}{s^2}}$

• Simplified:

True Δv = ( ( Δv atm - 1000 ) / Δv atm ) * Δv vac + 1000

• Explained:

True Δv = ( ( Total Δv in atmosphere - 1000 m/s2) / Total Δv in atmosphere ) X Total Δv in vacuum + 1000

• Example:

Single Stage with total atmospheric Δv of 5000 m/s2, and rated 6000 Δv in vacuum.

Transitional Δv = ( ( 5000 Δv atm - 1000 Δv Required to escape Kerbin atmosphere ) / 5000 Δv atm ) X 6000 Δv vac + 1000 Δv Required to escape Kerbin atmosphere = Total Δv of 5800 m/s2

See also