Timeline for What propulsion methods does the ISS use for station-keeping?
Current License: CC BY-SA 3.0
7 events
| when toggle format | what | by | license | comment | |
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| Apr 12, 2014 at 21:06 | history | edited | Mark Adler | CC BY-SA 3.0 |
clarify
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| Apr 12, 2014 at 21:01 | comment | added | Mark Adler | For the ATV: "From the 7 tonnes of available propellant, approximately 2.3 tonnes is available for free flight manoeuvres and approximately 4.7 tonnes is available for manoeuvring the space station at intervals of 10 to 45 days." From that, the Isp of 2650 m/s, and the mass of the ATV and ISS, you can compute the $\Delta V$'s from the 2.3 and 4.7 metric tons of propellant respectively. | |
| Apr 12, 2014 at 20:57 | comment | added | osgx | How much delta-v does ATV or Progress have for themself? How much delta-v get ISS from them (0.5-2 m/s)? | |
| Apr 12, 2014 at 20:56 | history | edited | Mark Adler | CC BY-SA 3.0 |
add ATV
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| Apr 12, 2014 at 19:07 | vote | accept | Stu | ||
| Apr 12, 2014 at 18:38 | history | edited | Mark Adler | CC BY-SA 3.0 |
add frequency
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| Apr 12, 2014 at 18:33 | history | answered | Mark Adler | CC BY-SA 3.0 |