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  • ...or subtract to reach a desired new orbital altitude. To do this, use the formula below to determine the target velocity for your initial burn: In this formula, ''r<sub>l</sub>'' and ''r<sub>h</sub>'' are the radii of the lower and hig
    9 KB (1,474 words) - 19:52, 2 May 2019
  • The relation between orbital speed and acceleration is given by the formula: ...depending on your distance from the planet, so we also need the following formula to determine ''a'' based on your altitude:
    6 KB (1,227 words) - 19:50, 2 May 2019
  • ...e, but it depends on the definition of which average distance is meant. In formula the semi-major axis is usually abbreviated by a lowercase <tt>a</tt> which
    16 KB (2,581 words) - 00:21, 6 February 2025
  • ...e orbit). The apsides are usually given from the body's surface while most formula require the distance from the center of the body so the radius usually need :A general formula for the Delta-v of a vehicle with thrust ''T'' and mass ''m'',
    23 KB (3,789 words) - 18:25, 21 June 2021
  • == Formula == {{Formula|math=\text{TWR} = \frac{F_T}{m \cdot g} > 1|where=* <math>F_T</math> è la
    8 KB (1,257 words) - 14:21, 23 August 2016
  • ...p;km orbit and then boost into a 200&nbsp;km orbit. Both circularized. The formula for the first burn is the following: This is the formula for the final burn in the transfer:
    11 KB (2,036 words) - 21:56, 24 July 2019
  • {{Formula|math=m_\text{fuel} = V_\text{fuel} \cdot \rho_\text{fuel}|where=*<math>m_\t {{Formula|math=\begin{align}
    11 KB (1,904 words) - 09:12, 17 March 2023
  • {{Formula|math=\frac{F_T}{W}=\frac{F_T}{m \cdot g_0}|where=* <math>F_T</math> jest to {{Formula|math code=<math>I_{sp} = \frac{T}{\dot m \cdot g_0}, [I_{sp}] = s</math> <s
    3 KB (544 words) - 12:59, 19 August 2018
  • The efficiency produced by solar panels can be calculated using the formula:
    7 KB (1,009 words) - 01:34, 24 March 2025
  • {{Formula|math=r = \frac{1}{p}|where=* <math>r</math> is the revolutions per time uni {{Formula|math=p_\text{synodic} = \left\vert\frac{1}{\frac{1}{p_t} - \frac{1}{p_o} }\
    9 KB (1,046 words) - 12:47, 6 November 2021
  • I use such formula to calculate: '''Channels * (Depth/8) = Bytes / (Length * Width)'''
    4 KB (666 words) - 04:14, 24 July 2024
  • ...erage]] can what altitude is needed for an amount of given satellites. The formula to calculate the distance between two satellites is important to select the
    7 KB (1,133 words) - 20:21, 2 May 2019
  • == Formula == {{Formula|math=\text{TWR} = \frac{F_T}{m \cdot g} > 1|where=* <math>F_T</math> is the
    7 KB (1,245 words) - 12:42, 29 April 2023
  • ...le the eye have to turn to look from one side of an object to another. The formula to calculate this for a sphere is: <math>\delta = 2 \cdot arcsin\left(\frac
    4 KB (647 words) - 14:55, 25 December 2024
  • {{Formula|math=I_{sp} = \frac{F_T}{\dot m}|where=* <math>I_{sp}</math> is the specifi {{Formula|math=I_{sp,g_0} = \frac{F_T}{\dot m \cdot g_0} = \frac{I_{sp} }{g_0}|where
    10 KB (1,718 words) - 02:29, 3 January 2023
  • ...or subtract to reach a desired new orbital altitude. To do this, use the formula below to determine the target velocity for your initial burn: In this formula, ''r<sub>l</sub>'' and ''r<sub>h</sub>'' are the radii of the lower and hig
    11 KB (1,356 words) - 18:38, 2 May 2019
  • ...ites (if their angular distance is known) can be calculated with following formula: ...e connection between the satellites. To calculate the height the following formula can be used:
    4 KB (687 words) - 20:23, 2 May 2019
  • ...to calculate what altitude you need [skip to the end for answer]. Use the formula r = k·T<sup>2/3</sup> where r is the radius of the circular orbit [actuall
    11 KB (1,675 words) - 03:51, 1 March 2022
  • * This formula works for all (circular) orbits, as <tt>t</tt> isn't given; <tt>a</tt> is t ...evel of the planet, and <math>R_p</math> is the radius of the planet. This formula calculates the altitude above sea level for any given orbital period <math>
    4 KB (720 words) - 22:04, 19 May 2017
  • {{Formula|math=\text{TWR} = \frac{F_T}{m \cdot g} > 1|where=* <math>F_T</math> is the {{Formula|math=\Delta{v} = ln\left(\frac{M_{start} }{M_{end} }\right) \cdot I_{sp} \c
    11 KB (1,728 words) - 20:14, 25 July 2024

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