![]() |
|
|
Thread Tools | Display Modes |
#11
|
|||
|
|||
![]()
The problem is that I want to launch an unmanned rocket, and I want to
be sure I learn why it dies, if it dies. It would be a "bad thing" to spend millions (or at least hundreds of thousands) to launch a rocket - and learn nothing from it! -David |
#12
|
|||
|
|||
![]()
Ian Stirling wrote:
Len wrote: David Summers wrote: So, assuming that we can build an orbital vehicle, get a launch permit, etc - what is the best (or cheapest) method of tracking the vehicle after launch? ...snip.... Unless the government requires close and continuous tracking, I fail to see the urgency. When I learned to fly a little It's very nice to have more-or-less continuous tracking and data relay if you are not sure of the device, or even if you are, and things go wrong. over six decades ago, the pilot navigated and told anyone interested on the ground the aircraft's position. Perhaps If you've got a pilot onboard, some of the problems go away (as long as the pilot can communicate the problem to the ground in some manner), but for stuff like finding out on orbit that somebody put in the solar array extend motor in backwards, and you need to try reversing it before the batteries run out, rapid comms is pretty much essential. I'm oriented toward a commercial space transportation system where the cargo should not dominate the mission. Even though transportation costs have come down from $1 million per lbm to perhaps $5k per lbm, we still seem to be spending as much as $50 per lbm on payload. This really becomes absurd, when transportation costs get down to perhaps $100 per lbm. At some point, the cost of the payload should be commensurate with the cost of transporting it. When that happens, the perspective should change with respect to how much one should pay for knowledge of what happened--rather than simply replacing the cargo and flying it again. At some point we may stop putting the "cargo in front of the horse." Best regards, Len (Cormier) PanAero, Inc. (change x to len) http://www.tour2space.com |
#13
|
|||
|
|||
![]()
On Mon, 21 Feb 2005 03:36:26 +0000, Andrew Gray wrote:
Incidentally, a recent post on sci.space.history mentioned a couple of Gemini research papers, which involved injecting water into the plasma sheath during re-entry - FLIGHT INVESTIGATION AND ANALYSIS OF ALLEVIATION OF COMMUNICATIONS BLACKOUT BY WATER INJECTION DURING GEMINI 3 REENTRY By Lyle C. Schroeder and Francis P. Russo Langley Research Center A method of overcoming reentry communications blackout by injecting water into the flow field was demonstrated during the Gemini-Titan 3 (GT-3) mission. Significant levels of signal strength increase during the early portion of the water injection sequence over an altitude range from 272000 to 246000 ft (82.90 to 74.98 km) were noted by ground stations on VHF telemetry (230.4 MHz) and VHF voice (296.8 MHz). Interesting, I'd guess it cools the plasma so that it's not plasma anymore and probably works best when the density of the plasma is low. You could reduce the amount of water necessary by only injecting water into the flow every so often to get a state update. Craig Fink |
#14
|
|||
|
|||
![]() Len wrote: Ian Stirling wrote: Len wrote: David Summers wrote: So, assuming that we can build an orbital vehicle, get a launch permit, etc - what is the best (or cheapest) method of tracking the vehicle after launch? ...snip.... Unless the government requires close and continuous tracking, I fail to see the urgency. When I learned to fly a little It's very nice to have more-or-less continuous tracking and data relay if you are not sure of the device, or even if you are, and things go wrong. over six decades ago, the pilot navigated and told anyone interested on the ground the aircraft's position. Perhaps If you've got a pilot onboard, some of the problems go away (as long as the pilot can communicate the problem to the ground in some manner), but for stuff like finding out on orbit that somebody put in the solar array extend motor in backwards, and you need to try reversing it before the batteries run out, rapid comms is pretty much essential. I'm oriented toward a commercial space transportation system where the cargo should not dominate the mission. Even though transportation costs have come down from $1 million per lbm to perhaps $5k per lbm, we still seem to be spending as much as $50 per lbm on payload. oops. Somewhere I lost three zeros. This was supposed to be $50k per lbm on payload. Len This really becomes absurd, when transportation costs get down to perhaps $100 per lbm. At some point, the cost of the payload should be commensurate with the cost of transporting it. When that happens, the perspective should change with respect to how much one should pay for knowledge of what happened--rather than simply replacing the cargo and flying it again. At some point we may stop putting the "cargo in front of the horse." Best regards, Len (Cormier) PanAero, Inc. (change x to len) http://www.tour2space.com |
#15
|
|||
|
|||
![]()
Len wrote:
I'm oriented toward a commercial space transportation system where the cargo should not dominate the mission. Even though transportation costs have come down from $1 million per lbm to perhaps $5k per lbm, we still seem to be spending as much as $50 per lbm on payload. ITYM $50k per ... This really becomes absurd, when transportation costs get down to perhaps $100 per lbm. [ $48/lb (to equatorial LEO) ($950,000 for 9 metric tons cargo) ] At some point, the cost of the payload should be commensurate with the cost of transporting it. Yeaaay!! Right on. It's a qualitative difference though, not just a quantitive one. And the money men aren't used to it. Your sat fails? send another one up. In fact, send up another one anyway, just in case the first one fails. Or send two spares up, why not? Your sat goes through 4 design evolutions at $5 million each? Send it up after one and see if it works, and how well. Better, just do a half-assed design and test that ... No, don't just divide the cost per sat by 10, divide it by 100. Your new sat now costs $500,000, not $50 million. You might need two ... total, including launch, about the cost of a nice small house. Or worse, the new sat, with the same capability, now costs $50,000 ... Thing is, after some recent talks with a major sat operator/capital guy, if you do that then their present fleet of comsats has to be devalued - which affects their balance sheet adversely. Which makes the owners of the present fleet of comsats a bit unwilling to invest in launch capacity, or to encourage others to do so. And as they are regarded by the Banks as the only people with space financial expertise ... ... no-one is really eager to invest the required large sums needed for realistic CATS*. like buying the newest computer - after a few years it will be worth nothing. And for the operators, those few years are now, and unexpectedly, shorter then the projected lifetime of the existing sats - or would be, if there was a CATS. *100 or two million is not enough for CATS, you'd need a bit more than one billion to start, and ten billion would be a realistic minimum to control a major share of the long term market, assuming governments would intervene and try to compete later. Of course the exclusivity of owning a sat wasn't mentioned: "I have a Sat, and control some media, and you don't; but is that important?" Like: "I have $5 billion, and you don't" wasn't mentioned either. There is a doctrine that sats should be environmentally disposed of from GEO at the end of their lives. I wonder if someone might now get a contract to collect them at some point near (or in) GEO, which would be easier on their remaining fuel than the alternative burn, and just store them until their value as mass (or as scrap) was optimum? So who's actually doing it all? I'm not ... yet -- Peter Fairbrother |
#16
|
|||
|
|||
![]()
"David Summers" :
The problem is that I want to launch an unmanned rocket, and I want to be sure I learn why it dies, if it dies. It would be a "bad thing" to spend millions (or at least hundreds of thousands) to launch a rocket - and learn nothing from it! That is what 'Black Boxes' are for. Earl Colby Pottinger -- I make public email sent to me! Hydrogen Peroxide Rockets, OpenBeos, SerialTransfer 3.0, RAMDISK, BoatBuilding, DIY TabletPC. What happened to the time? http://webhome.idirect.com/~earlcp |
#17
|
|||
|
|||
![]()
On 2005-02-22, Peter Fairbrother wrote:
There is a doctrine that sats should be environmentally disposed of from GEO at the end of their lives. I wonder if someone might now get a contract to collect them at some point near (or in) GEO, which would be easier on their remaining fuel than the alternative burn, and just store them until their value as mass (or as scrap) was optimum? I believe that whilst deorbiting is popular as disposal for LEO satellites, it's less so for GEO satellites - instead, they're moved into a stable orbit still some great distance out, but either higher or lower than the one they were in, and not intersecting with GEO. This keeps them out of trouble without needing to spend a great deal on providing enough fuel to deorbit them. -- -Andrew Gray |
#18
|
|||
|
|||
![]()
On 2005-02-22, Craig Fink wrote:
On Mon, 21 Feb 2005 03:36:26 +0000, Andrew Gray wrote: Incidentally, a recent post on sci.space.history mentioned a couple of Gemini research papers, which involved injecting water into the plasma sheath during re-entry - FLIGHT INVESTIGATION AND ANALYSIS OF ALLEVIATION OF COMMUNICATIONS BLACKOUT BY WATER INJECTION DURING GEMINI 3 REENTRY By Lyle C. Schroeder and Francis P. Russo Langley Research Center A method of overcoming reentry communications blackout by injecting water into the flow field was demonstrated during the Gemini-Titan 3 (GT-3) mission. Significant levels of signal strength increase during the early portion of the water injection sequence over an altitude range from 272000 to 246000 ft (82.90 to 74.98 km) were noted by ground stations on VHF telemetry (230.4 MHz) and VHF voice (296.8 MHz). Interesting, I'd guess it cools the plasma so that it's not plasma anymore and probably works best when the density of the plasma is low. You could reduce the amount of water necessary by only injecting water into the flow every so often to get a state update. Yeah, there's a couple of papers on NTRS about it (one report on the experiment, one description made beforehand); will hopefully get around to reading through them sometime soon. Doesn't say if much *data* was transmitted, mind you... It also only needs to be done to the area around the antennae, and even then the amount is limited; it certainly looked at first glance like a viable concept, although I guess it was felt to be more trouble than it was worth (especially since re-entry communications class as "nice, but not essential"). And these days, of course, it's a lot less critical what with TDRS and the like. -- -Andrew Gray |
#19
|
|||
|
|||
![]()
True, but the Earth is a big place - and with no telemetry there would
be a lot of places to check. Most likely it would hit ocean and sink, so having it "phone home" would be unreliable at best. I want to know what happened (as in what failure caused deorbit), when it happened, and where the vehicle ended up. -David |
#20
|
|||
|
|||
![]()
Peter Fairbrother wrote:
Len wrote: I'm oriented toward a commercial space transportation system where the cargo should not dominate the mission. Even though transportation costs have come down from $1 million per lbm to perhaps $5k per lbm, we still seem to be spending as much as $50 per lbm on payload. ITYM $50k per ... Yes, an error I caught in a later message. This really becomes absurd, when transportation costs get down to perhaps $100 per lbm. [ $48/lb (to equatorial LEO) ($950,000 for 9 metric tons cargo) ] At some point, the cost of the payload should be commensurate with the cost of transporting it. Yeaaay!! Right on. It's a qualitative difference though, not just a quantitive one. And the money men aren't used to it. Your sat fails? send another one up. In fact, send up another one anyway, just in case the first one fails. Or send two spares up, why not? Your sat goes through 4 design evolutions at $5 million each? Send it up after one and see if it works, and how well. Better, just do a half-assed design and test that ... No, don't just divide the cost per sat by 10, divide it by 100. Your new sat now costs $500,000, not $50 million. You might need two ... total, including launch, about the cost of a nice small house. Or worse, the new sat, with the same capability, now costs $50,000 ... Thing is, after some recent talks with a major sat operator/capital guy, if you do that then their present fleet of comsats has to be devalued - which affects their balance sheet adversely. Which makes the owners of the present fleet of comsats a bit unwilling to invest in launch capacity, or to encourage others to do so. And as they are regarded by the Banks as the only people with space financial expertise ... ... no-one is really eager to invest the required large sums needed for realistic CATS*. like buying the newest computer - after a few years it will be worth nothing. And for the operators, those few years are now, and unexpectedly, shorter then the projected lifetime of the existing sats - or would be, if there was a CATS. *100 or two million is not enough for CATS, you'd need a bit more than one billion to start, and ten billion would be a realistic minimum to control a major share of the long term market, assuming governments would intervene and try to compete later. Lots of good thoughts and analysis, Peter. I pretty much agree with what you have said. However, I do think that $200 million could be enough for a space transport system capable of carrying about one tonne at a time. One just needs to be somewhat clever about the design and the development plan. The need for big money comes afterward to pay for the application--e.g. 4000 LEO comsats at $1 million each for manufacture and launch. However, I think the big money can come once you have a space transport operational and have shown proof of concept for the ap. Big LEO comsats have never been tried in a proper way. Done right, the economics and performance can be truly compelling. Of course the exclusivity of owning a sat wasn't mentioned: "I have a Sat, and control some media, and you don't; but is that important?" Like: "I have $5 billion, and you don't" wasn't mentioned either. There is a doctrine that sats should be environmentally disposed of from GEO at the end of their lives. I wonder if someone might now get a contract to collect them at some point near (or in) GEO, which would be easier on their remaining fuel than the alternative burn, and just store them until their value as mass (or as scrap) was optimum? Perhaps another good ap--once you have the space transport. Best regards, Len (Cormier) PanAero, Inc. (change x to len) http://www.tour2space.com So who's actually doing it all? I'm not ... yet -- Peter Fairbrother |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Space Access Update #108 1/31/05 | Henry Vanderbilt | Policy | 0 | February 1st 05 05:56 PM |
Lockheed Martin Crew Exploration Vehicle team includes top industry innovators | Jacques van Oene | Space Shuttle | 0 | January 31st 05 02:51 PM |
Gravity as Falling Space | Henry Haapalainen | Science | 1 | September 4th 04 04:08 PM |
Space Access Update #102 2/9/04 | Henry Vanderbilt | Policy | 1 | February 10th 04 03:18 PM |
International Space Station Science - One of NASA's rising stars | Jacques van Oene | Space Station | 0 | December 27th 03 01:32 PM |