Of course, in the period between Dragon escape capability being introduced and Dragon propulsive landing being introduced, Dragon will carry excess propellant to the ISS that could be used for reboost.
Suffredini said that Dragon may carry 800 lbs of cargo on COTS 2.
Why not carry a more CRS-sized load?
Quote from: corrodedNut on 08/24/2011 12:56 pmHardware, lots and lots of hardware:http://www.nasa.gov/pdf/580727main_4%20-%20Lindenmoyer%20COTS%20Status_508.pdfLovely pictures.I do see that there is at least the "starboard" window, here to the right of the hatch. Perhaps the other window is there too, now uncovered by what may have been something temporary. The suface looks different than in the pervious photos.
Hardware, lots and lots of hardware:http://www.nasa.gov/pdf/580727main_4%20-%20Lindenmoyer%20COTS%20Status_508.pdf
Quote from: Jason1701 on 08/24/2011 05:31 pmSuffredini said that Dragon may carry 800 lbs of cargo on COTS 2. I've seen others on twitter report 800 kg. Which is is then?
Quote from: starsilk on 08/24/2011 04:53 pm1. I'm not sure I'd agree that the capability is 'not required'. there have been plans for a (US) ISS reboost module to cover the possibility of the Russian segment (or vehicles) being unable to do the job.2. seems like doing the work to 'certify' one of the new commercial US vehicles to do the job would be prudent (and it may be that Cygnus is better suited to the task, due to its shape).1. That was eons ago and not applicable to today.
1. I'm not sure I'd agree that the capability is 'not required'. there have been plans for a (US) ISS reboost module to cover the possibility of the Russian segment (or vehicles) being unable to do the job.2. seems like doing the work to 'certify' one of the new commercial US vehicles to do the job would be prudent (and it may be that Cygnus is better suited to the task, due to its shape).
2. No, not if it is not viable.
a. shape has nothing to do with one or the other
b. They don't carry propellant for reboost, only enough to do their mission.
1. well I'd say it's clearly more applicable *today* than it was ten years ago. now there's no Shuttle, no Progress (for a while), no ATV (for a while). that doesn't leave a whole heap of options. the onboard thruster is only useful as a very temporary solution, because it will wear out. it seems sensible to me to have a US solution for reboost.2. we won't know if it's viable until someone crunches the numbers.3. cygnus shape is better because it's thrusters don't need to be angled.4. add more propellant! there's obviously room for more in Dragon - the next COTS mission is carrying enough to do various exercises before actually docking. you have to assume Dragon is also being redesigned with bigger tanks *right now* to support their LAS solution. I'm sure cygnus could carry more too with a little redesign.
Yes, Dragon is not equiped with that capability and neither is ISS equiped with the ability to get prop from the US segment and transfer it to the Russian segment.Reboosting with Dragon from a CBM introducing many, many questions that need to be resolved (stress on stack, maneuver to attitude and power generation/cooling concerns, etc) at rather high cost and effort when it is not required.As I mentioned earlier, ISS reboost can be performed with the Russian segment thrusters.
add more propellant! there's obviously room for more in Dragon - the next COTS mission is carrying enough to do various exercises before actually docking. you have to assume Dragon is also being redesigned with bigger tanks *right now* to support their LAS solution. I'm sure cygnus could carry more too with a little redesign.
When you compare the orbital deal to the spacex deal, just how much more are we paying for orbital cargo compared to spacex cargo?
Quote from: corrodedNut on 08/24/2011 12:56 pmHardware, lots and lots of hardware:http://www.nasa.gov/pdf/580727main_4%20-%20Lindenmoyer%20COTS%20Status_508.pdfLovely pictures.I do see that there is at least the "starboard" window, here to the right of the hatch. Perhaps the other window is there too, now uncovered by what may have been something temporary. The suface looks different than in the pervious photos.And look at that unpresurized volume. How they plan to fit the LAS Super Dracos in there is beyond me.
In 2 years we could have VASIMR reboosting the ISS. How likely that really is I wouldn't know.
The only word from NASA has been that they had a budget of 800kg for cargo to the station in the combined COTS2/3 flight, but they were probably not going to use all of it. The Progress failure might however make them use up more of that.That's what I understood from the NASA press conference yesterday.