Revision as of 06:03, 25 June 2013

Introduction

Kerbal Space Program's Rocket Scientist Cheat Sheet Delta V Maps and Equations for Your Reference So You Can Get From Here to There and Back Again.

Delta V Maps

Various maps developed by KSP fans.

• dV Total Values

1. http://wiki.kerbalspaceprogram.com/w/images/7/73/KerbinDeltaVMap.png
2. http://www.skyrender.net/lp/ksp/system_map.png

• dV Change Values

1. http://i.imgur.com/duY2S.png

• dV KSP Nomogram

1. http://ubuntuone.com/1kD39BCoV38WP1QeG6MtO6

Thrust to Weight Ratio (TWR)

1. This is Newton's Second Law.
2. If ratio is less than 1, you will not lift off the ground.

• Equation:

TWR = F / (m * g) > 1

• Explained:

TWR = Force of Thrust / ( Total Mass X 9.81 ) > 1

• Example:

200 kiloNewton rocket engine on a 15 ton rocket launching from Kerbin Space Center.

TWR = 200 kN / ( 15 Tons total Mass X 9.81 m/s2 ) = 1.36 which is > 1 which means liftoff!

Combined Specific Impulse (Isp)

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

• Equation:

Isp = ( F1 + F2 + ... ) / ( ( F1 / Isp1 ) + ( F2 / Isp2 ) + ... )

• Explained:

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

• Example:

Two engines, one rated 200 Newtons and 120 Specific Impulse; another engine rated 50 Newtons and 200 Specific Impulse.

Isp = (200 Netwons + 50 Newtons) / ( ( 200 Newtons / 120 ) + ( 50 Newtons / 200 ) = 130.89 Specific Impulse

Delta V (dV)

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

• Equation:

dV = ln ( Mstart / Mend ) * Isp * g

• Explained:

dV = ln ( Starting Mass / Ending Mass ) X Isp X 9.81

• Example:

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

dV = ln ( 23 Tons / 15 Tons ) X 120 Specific Impulse X 9.81m/s = Total dV of 1803.2 m/s2

Transitional Delta V (dV) aka True dV when launching from Kerbin (a stupid_chris contribution)

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

• Equation:

TdV = ( ( dVatm - 1000 ) / dVatm ) * dVvac + 1000

• Explained:

Transitional dV = ( ( Total dV in atmosphere - 1000 m/s2) / Total dV in atmosphere ) X Total dV in vacuum + 1000

• Example:

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

Transitional dV = ( ( 5000 dVatm - 1000 dV Required to escape Kerbin atmosphere ) / 5000 dVatm ) X 6000 dVvac + 1000 dV Required to escape Kerbin atmosphere = Total dV of 5800 m/s2

Libraries

Links to libraries of reference materials. Please refer to Tutorials for for information on specific tutorials not linked in these libraries.

• The Drawing Board: A library of tutorials and other useful information