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fixed minor typos
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Brian Tompsett - 汤莱恩
Brian Tompsett - 汤莱恩
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Variant of the Tsiolkovsky rocket equation including engine specficspecific power and efficiency, can anyone help me under stand how this works

enter image description here

firstFirst of all this code is not mine iI am trying to understand how the equation for m_u works. thisThis comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovskyTsiolkovsky rocket equation iI believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. canCan anyone link to elsewhere this equation can be found?

toTo make it clearer the equation is enter image description here

whereWhere Ve is (Isp * Gravity constant).

linkLink to thesis is https://webthesis.biblio.polito.it/15184/1/tesi.pdf

Variant of the Tsiolkovsky rocket equation including engine specfic power and efficiency, can anyone help me under stand how this works

enter image description here

first of all this code is not mine i am trying to understand how the equation for m_u works. this comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovsky rocket equation i believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. can anyone link to elsewhere this equation can be found

to make it clearer the equation is enter image description here

where Ve is (Isp * Gravity constant)

link to thesis is https://webthesis.biblio.polito.it/15184/1/tesi.pdf

Variant of the Tsiolkovsky rocket equation including engine specific power and efficiency, can anyone help me under stand how this works

enter image description here

First of all this code is not mine I am trying to understand how the equation for m_u works. This comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the Tsiolkovsky rocket equation I believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. Can anyone link to elsewhere this equation can be found?

To make it clearer the equation is enter image description here

Where Ve is (Isp * Gravity constant).

Link to thesis is https://webthesis.biblio.polito.it/15184/1/tesi.pdf

added 73 characters in body
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Gwyn Davies
Gwyn Davies
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enter image description here

first of all this code is not mine i am trying to understand how the equation for m_u works. this comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovsky rocket equation i believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. can anyone link to elsewhere this equation can be found

to make it clearer the equation is enter image description here

where Ve is (Isp * Gravity constant)

link to thesis is https://webthesis.biblio.polito.it/15184/1/tesi.pdf

enter image description here

first of all this code is not mine i am trying to understand how the equation for m_u works. this comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovsky rocket equation i believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. can anyone link to elsewhere this equation can be found

to make it clearer the equation is enter image description here

where Ve is (Isp * Gravity constant)

enter image description here

first of all this code is not mine i am trying to understand how the equation for m_u works. this comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovsky rocket equation i believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. can anyone link to elsewhere this equation can be found

to make it clearer the equation is enter image description here

where Ve is (Isp * Gravity constant)

link to thesis is https://webthesis.biblio.polito.it/15184/1/tesi.pdf

added 124 characters in body
Source Link
Gwyn Davies
Gwyn Davies
  • 113
  • 5

enter image description here

first of all this code is not mine i am trying to understand how the equation for m_u works. this comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovsky rocket equation i believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. can anyone link to elsewhere this equation can be found

to make it clearer the equation is enter image description here

where Ve is (Isp * Gravity constant)

enter image description here

first of all this code is not mine i am trying to understand how the equation for m_u works. this comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovsky rocket equation i believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. can anyone link to elsewhere this equation can be found

enter image description here

first of all this code is not mine i am trying to understand how the equation for m_u works. this comes from a master thesis called Trajectory design for a Titan mission using the Direct Fusion Drive as shown it is a different variant of the tsiolkovsky rocket equation i believe for the propellant weight on the rocket in this case it is being used to plot the change in delta V relevant to mission length so Delta-t is total number of seconds in 0 to 15 years. can anyone link to elsewhere this equation can be found

to make it clearer the equation is enter image description here

where Ve is (Isp * Gravity constant)

Source Link
Gwyn Davies
Gwyn Davies
  • 113
  • 5