Author Topic: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)  (Read 265115 times)

Offline Jim

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #880 on: 04/05/2007 12:31 pm »
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wingod - 4/4/2007  12:05 AM

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aero313 - 2/4/2007  1:02 PM

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Cretan126 - 2/4/2007  11:30 AM

 Has anyone noted that LockMart builds the Atlas V EELV - in its entirety - at its facility at the foot of the Rocky Mountains in Littleton, CO?  Not a port in sight.  They transport the booster (in the early morning hours) from Littleton to Denver International and fly them to the Cape or VAFB.  So being near a port is not that big of a deal, although it helps.

Free air freight on government-furnished C-5As probably doesn't hurt either.

Let's be serious here.  The decisions made by a company with a lot of legacy infrastructure and overhead costs being primarily carried on government contracts will be made differently than those of a purely commecial, supposedly "clean sheet" company whose stated goal is low cost launch.  The location of the Martin Waterton plant was driven as much by Cold War-driven dispersion of national assets as anything else.  Building Delta IIs in Pueblo, CO also made sense when you factored in goverment surplus facilities, incentives, etc.

They only built the D-II upper stage there.


The whole Delta II was built in Pueblo

Offline aero313

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #881 on: 04/05/2007 04:04 pm »
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Jim - 5/4/2007  8:31 AM

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wingod - 4/4/2007  12:05 AM

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aero313 - 2/4/2007  1:02 PM

Let's be serious here.  The decisions made by a company with a lot of legacy infrastructure and overhead costs being primarily carried on government contracts will be made differently than those of a purely commecial, supposedly "clean sheet" company whose stated goal is low cost launch.  The location of the Martin Waterton plant was driven as much by Cold War-driven dispersion of national assets as anything else.  Building Delta IIs in Pueblo, CO also made sense when you factored in goverment surplus facilities, incentives, etc.

They only built the D-II upper stage there.


The whole Delta II was built in Pueblo

Actually, weren't the tanks built at Huntington Beach, with stage assy at Pueblo?  I recall that GEMs were stored in bunkers at Pueblo also.  Of course, final assy and checkout of the vehicle took place at CCAFS or VAFB.

Offline Jim

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #882 on: 04/05/2007 04:10 pm »
Ok, the Delta II components:  first stage, second stage, interstage, and 9.5 ft fairing were assembled in Pueblo

Offline BarryKirk

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #883 on: 04/05/2007 05:05 pm »
Getting back to the original topic sort of...

Any word on the publishing of the Falcon 9 user manual and/or a more exact date for the next Falcon 1 launch other than Q3 2007?

Offline wingod

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #884 on: 04/05/2007 05:56 pm »
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Jim - 5/4/2007  7:31 AM

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wingod - 4/4/2007  12:05 AM

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aero313 - 2/4/2007  1:02 PM

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Cretan126 - 2/4/2007  11:30 AM

 Has anyone noted that LockMart builds the Atlas V EELV - in its entirety - at its facility at the foot of the Rocky Mountains in Littleton, CO?  Not a port in sight.  They transport the booster (in the early morning hours) from Littleton to Denver International and fly them to the Cape or VAFB.  So being near a port is not that big of a deal, although it helps.

Free air freight on government-furnished C-5As probably doesn't hurt either.

Let's be serious here.  The decisions made by a company with a lot of legacy infrastructure and overhead costs being primarily carried on government contracts will be made differently than those of a purely commecial, supposedly "clean sheet" company whose stated goal is low cost launch.  The location of the Martin Waterton plant was driven as much by Cold War-driven dispersion of national assets as anything else.  Building Delta IIs in Pueblo, CO also made sense when you factored in goverment surplus facilities, incentives, etc.

They only built the D-II upper stage there.


The whole Delta II was built in Pueblo

Sorry but nope.  At least until the late 90's.  I had a tour of the facility in Huntington Beach where the First stage of the D-II was built out of the aluminium blanks.  I saw the blanks turned into a stage there.  They also were doing the Titan IV fairing there.

They may have sent it to Pueblo for some assembly but the stage was actually built in California.

They always had problems with corrosion due to the proximity to the ocean there.


Offline Jim

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #885 on: 04/05/2007 06:18 pm »
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wingod - 5/4/2007  1:56 PM

They may have sent it to Pueblo for some assembly but the stage was actually built in California.

They always had problems with corrosion due to the proximity to the ocean there.


In the 2000's, HB did no assembly of stages.   Tank mate, centerbody construction, engine section construction, engine installation and wiring was done in Pueblo.  That maybe applies since the 90's too.  

Tank construction is a different thing.  Much like San Diego building Centaur tanks but Denver assembles the Centaur.

D-II second stage tanks build was moved from HB to Italy
D-II 1st tanks were moved to Decatur from TBD.  There may have been a short time in Pueblo after HB

Offline aero313

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #886 on: 04/05/2007 07:18 pm »
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Jim - 5/4/2007  2:18 PM

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wingod - 5/4/2007  1:56 PM

They may have sent it to Pueblo for some assembly but the stage was actually built in California.

They always had problems with corrosion due to the proximity to the ocean there.


In the 2000's, HB did no assembly of stages.   Tank mate, centerbody construction, engine section construction, engine installation and wiring was done in Pueblo.  That maybe applies since the 90's too.  

Tank construction is a different thing.  Much like San Diego building Centaur tanks but Denver assembles the Centaur.

Jim is correct.  I spent several months at HB in 1995 during the Med-Lite proposal activity.  Even then, tank assy (and only tank assy) was done at HB.  Everthing else got shipped to and integrated at Pueblo.

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #887 on: 04/05/2007 08:23 pm »

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wingod - 4/4/2007  11:24 PM The problem with the small sat market is the cost/benefit ratio.

Wingod, thanks for the attempt at a market justification. When you look at financing a new business activity, its a lot more complex than just a cost/benefit ratio, because the risk always outweighs the small advantage you start off with.

To begin with, you look at comparative history, because the decisions are made looking at the history of what has been done before as a model of what will happen. Most of the LV's we now have (Atlas, Delta) had large portions of development at cost plus as military vehicles, so they make for lousy models. Strike one against doing a small sat market LV, where we don't have history. If you were to account for the total development of past vehicles with dependencies, they are all massively unprofitable.

Next,  we need to have a market opportunity that will be permanent and doesn't get subsumed into another segment. Having a cluster of small sats launch as part of another program, like recently with Orbital Express, undercuts the segmentation of small sats and smart sat LV markets, because its more convenient to account for them as offsets to a program rather than as components of a distinct market segment. Even if you could justify something like a low budget Iridium to generate a need for a volume in the market, it would likely be the case to be accounted for as if it were a single or few "big things" of standard treatment. So the big problem with creating a new market segment is the fight for definition, as it tends to sublimate away. We've gotten nowhere near a satisfactory return scenario, because the market itself is too insignificant.

A better case might be made for fast response, as Falcon 1 is justified. However, Jim already correctly challenged this by pointing out how much needs to happen for such to be brought off. In this case, its not market or cost effectiveness that kill you, but operational performance in delivering the fast response launch capability.


Offline rpspeck

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #888 on: 04/05/2007 08:58 pm »
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nobodyofconsequence - 5/4/2007  2:15 PM

No. Space-X won't disrupt the LV market - its too incestuous with its customers for that to happen.


You make some excellent points.  But I was specifically addressing future markets, involving customers currently “locked out” of space.  Customers similarly locked out of innovative computer work (by high prices) had an unexpectedly large impact in the years after 1976!

Offline aero313

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #889 on: 04/05/2007 09:13 pm »
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nobodyofconsequence - 5/4/2007  4:23 PM

A better case might be made for fast response, as Falcon 1 is justified.


Once again, please let's not confuse a countdown recycle with true responsive launch.  The Falcon 1 recycle used a vehicle that had been previously integrated and tested over several months, including the removal and replacement of components.  This same vehicle had the payload previously mated and checked out.  It had the vehicle already installed on the launch pad and all interfaces checked out.  The range was already active and everyone was already on console.  The vehicle had been loaded with propellants and only a portion of these were emptied and refilled.  The mission profile had already been developed, verified, and loaded into the flight computer.  The first several hours of the countdown had already been performed.  

Despite what SpaceX claims, they DID NOT demonstrate "responsive launch".  The responsive launch that DARPA and the Air Force are looking for is 24-48 hours from cold start callup (without payload mated) to satellite in orbit.  All this recycle demonstrated is that SpaceX is capable of replicating what Atlas ICBMs were able to do in 1958.

Offline rpspeck

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #890 on: 04/05/2007 09:36 pm »
“major error in this is passengers don't want to be in a spacesuit for the whole flight.”

Additional note: I believe the U2 pilots spend a lot more than two hours suited up.

A more serious note:  Given the proven loss of life (Russian) from spacecraft depressurization and experience with fast and slow depressurization in less demanding aircraft situations, why has the manned spaceflight industry decided to reverse aviation standards and condemn participants to death following any hull failure, including serious leakage?  The large cross section of the pressure hull becomes an “Acceptable”, single point Fatal failure?   To buy into this scenario and then talk about “Risk” in a spacesuit makes very little sense.  To avoid the fatal single point failure, all astronauts need to stay in their pressure suits until they at least transfer to a more robust (probably double walled) low stress space station.

A mechanical “counter-pressure” suit with a well designed, multi-feed face mask could approach the fail safe redundancy of a modern SCUBA rig.  Current pressure suits resemble the dangerous 1930s diving dress.  

For two hour rendezvous, I assumed a more precision control system than used in Mercury/Atlas.  Probably a “Hot Dog” like the 486 used on ISS.  Plus I assumed use of GPS so you would know where you were.      


Re Ejection: You can eject from a rocket after engine shutdown (near apogee if still deep in the atmosphere) with a bungee cord plus your standard deployment mechanism (already in freefall).  It is hard to think in these terms since explosive “Flight Termination” has been more common than Thrust Termination.

Re Fireballs: I have the recent “Sea Launch” in mind compared to the Falcon flights.  I don’t reject the escape rocket, since it also scales with “capsule” mass and covers altitudes too low for simple parachute use.  

Richard P. Speck,    Micro-Space, Inc.

Offline Jim

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #891 on: 04/05/2007 10:13 pm »
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rpspeck - 5/4/2007  5:36 PM

“1.  major error in this is passengers don't want to be in a spacesuit for the whole flight.”

Additional note: I believe the U2 pilots spend a lot more than two hours suited up.

2.  A more serious note:  Given the proven loss of life (Russian) from spacecraft depressurization and experience with fast and slow depressurization in less demanding aircraft situations, why has the manned spaceflight industry decided to reverse aviation standards and condemn participants to death following any hull failure, including serious leakage?  The large cross section of the pressure hull becomes an “Acceptable”, single point Fatal failure?   To buy into this scenario and then talk about “Risk” in a spacesuit makes very little sense.  To avoid the fatal single point failure, all astronauts need to stay in their pressure suits until they at least transfer to a more robust (probably double walled) low stress space station.

3.  For two hour rendezvous, I assumed a more precision control system than used in Mercury/Atlas.  Probably a “Hot Dog” like the 486 used on ISS.  Plus I assumed use of GPS so you would know where you were.      

4.  Re Ejection: You can eject from a rocket after engine shutdown (near apogee if still deep in the atmosphere) with a bungee cord plus your standard deployment mechanism (already in freefall).  It is hard to think in these terms since explosive “Flight Termination” has been more common than Thrust Termination.


Richard P. Speck,    Micro-Space, Inc.

1.  U-2 pilots are a select group of people performing a national security mission.  They weren't John Q. Public, who would have an issue with spending a long time in a spacesuit.

2.  You have no idea what you are talking about.  Both Russian and American spacecraft use pressure suits for launch.  Once on orbit, the pressure shells of both spacecraft are just as good as the space stations.  If there is a leak, the life support system pumps in enough air to maintain pressure long enough to allow the crew to put on their suits.  Also, the space stations don't use double hulls.

3. It has nothing to with a computer.  It is sensors and thrusters and a capable LV.   GPS is not one of the sensors (radar, laser, LLL cameras, etc).  And as I stated before there isn't a 2 hour rendevous.

4.  No you can't bail out, especially near apogee because you will burn up also


Online Lee Jay

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #892 on: 04/05/2007 10:24 pm »
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Jim - 5/4/2007  4:13 PM
2.  You have no idea what you are talking about.  Both Russian and American spacecraft use pressure suits for launch.  Once on orbit, the pressure shells of both spacecraft are just as good as the space stations.  If there is a leak, the life support system pumps in enough air to maintain pressure long enough to allow the crew to put on their suits.  Also, the space stations don't use double hulls.

I thought the normal atmospheric leak-rate of the ISS was much lower than the leak rate of the Shuttle (I mean, without a salient leak of some type).  Is this untrue?

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #893 on: 04/05/2007 10:39 pm »

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rpspeck - 5/4/2007  3:58 PM  
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nobodyofconsequence - 5/4/2007  2:15 PM  No. Space-X won't disrupt the LV market - its too incestuous with its customers for that to happen.  
 You make some excellent points.  But I was specifically addressing future markets, involving customers currently “locked out” of space.  Customers similarly locked out of innovative computer work (by high prices) had an unexpectedly large impact in the years after 1976!

These are called "white space" opportunities, and are the hardest to justify for finance, because you never know at what level your total cost profile has to reach to get enough of them. Also, a long sales cycle, possibly indefinite ensues. No sane investor touches these, just mavericks that almost always lose their shirt.

As to computers, it occurred in phases, not all at once. How you financed silicon valley start-ups at the time was off of the easy to prove productivity improvements, and may of the ventures were seeded on less than $50k. Wozniak and Jobs built Apple 1 out of junk from a junk dealer FYI. I don't think this is a good comparison.  


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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #894 on: 04/05/2007 10:47 pm »
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aero313 - 5/4/2007  4:13 PM  
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nobodyofconsequence - 5/4/2007  4:23 PM

A better case might be made for fast response, as Falcon 1 is justified.

 Once again, please let's not confuse a countdown recycle with true responsive launch.

Could not agree more. I said *justified*, not *achieved*. As in "financially justified", i.e. what they are trying to achieve.

If they don't deal with the many issues needed to achieve true responsive launch, then Falcon I is just a stepping stone to Falcon 9, and they are simply trying to undercut Delta IV's business, and the responsive launch was a convenient sham.  


Offline spacedreams

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #895 on: 04/05/2007 11:06 pm »
The LV market is actually quite simple and is directly related to the satellite market. If you have a cheap satellite and are willing to take some risk in possibly losing that satellite you are going to look for the cheapest ride (i.e. student projects, experimental satellites, elements of constellations, etc ...). If you have a satellite that you are paying $1Billion+ on and failure is not an option, you will pay extra $$$ to launch on a vehicle with proven reliability and increased oversight.

The cost of a launch vehicle increases with the experience and capability of the engineers (also related to desirable location for company), quality of workmanship (experienced union backed technicians), technology utilized, amount of qualification and testing performed, process control overhead, and overhead due to oversight among other factors.

If you look at who would use the heavy lifters you are talking about big payloads and/or far reaching orbits. The satellites that would operate in this category are usually not cheap so they are most likely not going to simply pick the cheapest launch vehicle.  As for human spaceflight, it all depends on the individual. There are people in this world who drive Audis and people who drive GMCs. There are prices and consequences to each and a bit of practicality that plays into the decision. If I need to get across the country and I have enough money, I'll fly. If I have a lot of money I'll pop for first class. If I don't the cash I'll fly southwest or take a train or bus. It all depends on what it is worth to the customer

Offline Comga

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #896 on: 04/06/2007 03:19 am »
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BarryKirk - 5/4/2007  11:05 AM

Getting back to the original topic sort of...

Any word on the publishing of the Falcon 9 user manual ...
Nada.  I know of a request for the Falcon 5 manual that has morphed into a request for the Falcon 9 manual over the three years that it has been outstanding.  The answer is repeatedly "soon" or even "next week".  

On another topic, did anyone read the editorial in the April 2 Aviation Week titled "Keep the Faith with SpaceX"?  It includes the lines

"So there is no reason to be dismayed or dismissive about the latest flight of upstart SpaceX's Falcon 1 launch vehicle, even though it was, strictly speaking, the second "failure" in two missions."

and "We remain hopeful about this launcher and hope others will, too. Falcon 1 could yet prove to be a beginning to the era of reliable, low-cost access that space so desperately needs if it is to mature beyond an age of experiments, exploration and exorbitant expense."

The editorial is remarkably upbeat and encouraging.  Those who are being dismissive or arguing about single words like "operational" should note this opinion from people who are respected for and paid for their opinions on such matters.
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline braddock

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #897 on: 04/06/2007 10:02 am »
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nobodyofconsequence - 6/4/2007  1:30 AM
But it comes from the hard work both in business and engineering in confronting requirements and making things work across the board. Not from fantasy.

Just as a bit of a counter-balance, Micro-Space HAS flown liquid fueled hardware, and IS attempting to participate in the Lunar Lander Challenge.  I imagine Richard HAS put in more than his share of hard work.

This is way off topic for this thread.  If Richard is willing, I'll set up a Q&A thread for him to take questions about Micro-Space. (PM or e-mail me [email protected] )

Offline braddock

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Re: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #898 on: 04/06/2007 05:29 pm »
I've started a proper Q&A thread for Mr. Speck for him to answer questions.
http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=7416&posts=1#M127299

Offline James Lowe1

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RE: LIVE: SpaceX - Falcon I (Mk.II) NET March 20 (Attempt 2)
« Reply #899 on: 04/09/2007 02:33 am »
And I've moved a load of posts into that thread which seem to be related to all of that fun and games. We want to keep this on SpaceX and Falcon I.

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