![]() |
|
|
Thread Tools | Display Modes |
#1
|
|||
|
|||
![]() |
#2
|
|||
|
|||
![]()
In article ,
Josh Gigantino wrote: This is research for my books. Any help would be appreciated, for any currently available launchers, esp Soyuz, Proton and Delta. I'm trying to spec out how much fuel would be available from burned out rocket stages for use by robotic "scavengers" in the storyline... The usual rule of thumb, in the West at least, is that residual fuel left in the tanks and plumbing is 1% of the initial load. However, in the past some stages have specified more aggressive residual percentages, e.g. 0.5% for Titan II first stage, 0.25% for S-IV (and the S-IV, at least, typically beat the spec substantially). So you really need to know the individual vehicle. And it's information that often doesn't make it into the user's manual, alas, which means there is no recourse except to talk to the launch supplier. know how to find/calculate this info so that I can figure out how much delta-V they would have available. About the only thing you can do is read the user's manuals and see if they give a mass breakdown at cutoff. They are mostly available on-line. -- MOST launched 30 June; science observations running | Henry Spencer since Oct; first surprises seen; papers pending. | |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Landing of Soyuz TMA-3 descent vehicle | Jacques van Oene | Space Station | 0 | May 5th 04 11:23 PM |
Successful European DELTA mission concludes with Soyuz landing | Jacques van Oene | Space Station | 0 | May 1st 04 12:25 PM |
Decision on the Soyuz TMA-4 spacecraft prelaunch processing | Jacques van Oene | Space Station | 0 | April 1st 04 01:12 PM |
Soyuz TMA-2 update, 28-10-2003 | Jacques van Oene | Space Station | 0 | October 29th 03 06:31 PM |
Rockets not carrying fuel. | Robert Clark | Technology | 3 | August 7th 03 01:22 PM |