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  #11  
Old 08-17-2012, 12:44 AM
Jerry Irvine's Avatar
Jerry Irvine Jerry Irvine is offline
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Quote:
Originally Posted by luke strawwalker
so a five segment booster will be what, about 1.6 million pounds?? They were designed to be put together vertically in the VAB and then crawled out to the pads via the crawler and crawlerways and launched at 39A/B at KSC. New infrastructure elsewhere is going to need a whole new approach, and lifting individual segments weighing a lot more than a diesel locomotive and stacking them on the pad is going to require some heavy duty GSE... which won't come cheap...
Lookie.
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  #12  
Old 08-17-2012, 06:17 AM
Rocket Doctor Rocket Doctor is offline
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Why are we knocking the ATK Liberty BEFORE we know it's capability?

There are many players in this commercialization of the space program.

In my opinion, Space X isn't the "God of Rocketry", too much hype.

You talk about proven success, what about the Merlin shutdown ?

We should all be open minded and see what hapens.

It reminds me how Estes was knocked for whatever they did, right or wrong.They did their best to provide the kits and motors we all wanted.

I think the key to that discussion was the previous owner.
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  #13  
Old 08-17-2012, 06:44 AM
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Joe Wooten Joe Wooten is offline
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Quote:
Originally Posted by ManofSteele
Actually, using a proven, man-rated solid rocket booster for a first stage IS the a superior technical choice for a manned launch vehicle, as compared to the SpaceX Falcon 9 Merlin 1C (3 flights) and Merlin 1D (0 flights). Invoking "political pork" is a bit dishonest, when Liberty was rated higher in previous evaluations and still not awarded funding.

Matt
(currently employed by ATK and a real rocket scientist)


Actually, if the concept of "man rating" had been applied to the shuttle before 4/12/81, the first several flights would have been under remote control with no astronauts aboard. The SRB's and the SSME's had never been used together as a system before then, just independent static firing of the individual components. How could the Liberty been rated higher when the Vulcain engine has not been "man rated" and the 5 segment SRB has never been launched, much less "man rated"? Man rating the 5 segment SRB/modified Vulcain before it was ever launched sounds like statistical hand waving based upon prior use of similar (but not the same) components in other systems.

The Falcon 9 and the Dragon capsule have now had 3 flights without people aboard and has had good performance, which is one more flight than the more primitive Gemini system had before it was declared "man rated". The cost of the Falcon 9 launch has been posted by Space X, has ATK done so, and has the Liberty had any launches yet as a system?

I stated it looked like political pork and I stand by that statement. It is an attempt to get government funding to develop the system, whereas Space X developed the Falcon 9/Dragon on their own dime in hopes of getting some NASA contracts for cargo delivery and astronaut taxi service. Has ATK/EADS/Boeing decided to build 3 launchers and test them on their own money? Let them develop it in a manner similar to Space X and I'll withdraw that statement.



Joe
(No rocket scientist, just a hard-headed engineer)
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  #14  
Old 08-17-2012, 08:20 AM
Rocket Doctor Rocket Doctor is offline
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As you probably know, NASA had one billion dollars to give out in contracts. Space X received $440 million of that.

Boeing and one othere company that i never heard of before divided up the remaining funds.

What did ATK Liberty get from that "pie" NOTHING !
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  #15  
Old 08-17-2012, 09:05 AM
Jerry Irvine's Avatar
Jerry Irvine Jerry Irvine is offline
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Quote:
Originally Posted by Joe Wooten with the annoying avatar uttered
Man rating the 5 segment SRB/modified Vulcain before it was ever launched sounds like statistical hand waving . . .
All "man rating" is "statistical hand waving" because nobody has the financial budget to consume 20 units to do it right.

Quote:
Originally Posted by Rocket Doctor
As you probably know, NASA had one billion dollars to give out in contracts. Space X received $440 million of that. Boeing and one other company that I never heard of before divided up the remaining funds.


http://www.nasa.gov/centers/kennedy...e-20120803.html

CCiCap partners are:
-- Sierra Nevada Corporation, Louisville, Colo., $212.5 million
-- Space Exploration Technologies (SpaceX), Hawthorne, Calif., $440 million
-- The Boeing Company, Houston, $460 million

Sierra Nevada is the company who made the (unstable combustion) SS1 hybrid and is making the (unstable combustion) SS2 hybrid and makes one of the manned shuttle like vehicles hoping to be launched to space by somebody and paid for by somebody.

http://www.sncorp.com/
http://www.denverpost.com/breakingn...d-212-5-million
http://en.wikipedia.org/wiki/Dream_Chaser
http://en.wikipedia.org/wiki/SpaceDev
http://www.spaceflightnow.com/news/...09sierranevada/

http://en.wikipedia.org/wiki/SpaceShipTwo

Quote:
Originally Posted by Wikipedia
2007 test explosion

On 26 July 2007, an explosion occurred during an oxidizer flow test at the Mojave Air and Space Port, where early-stage tests were being conducted on SpaceShipTwo's systems. The oxidizer test included filling the oxidizer tank with 4,500 kg (10,000 pounds) of nitrous oxide, followed by a 15-second cold-flow injector test. Although the tests did not ignite the gas, three employees were killed and three injured, two critically and one seriously, by flying shrapnel.[25]

[edit] RocketMotorTwo testing

Between 2005 and 2009, Scaled Composites conducted numerous small-scale rocket tests to evaluate SpaceShipTwo's engine design. After settling on the RocketMotorTwo hybrid rocket design, the company began performing full-scale hot-fire rocket tests in April 2009.[26] As of July 2012, 14 full-scale tests have been successfully conducted.[3][26]


Research Jerry

Here is a photo of a stable running hybrid with considerably higher ISP too.


HTP-HTPB hybrid SL ISP 240 lb-seconds/lb. This one is 6" OD. Tests up to 18" OD have been successfully conducted.
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  #16  
Old 08-17-2012, 11:44 AM
Rocket Doctor Rocket Doctor is offline
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Great information Jerry

RD
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  #17  
Old 08-17-2012, 01:43 PM
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Joe Wooten Joe Wooten is offline
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Quote:
Originally Posted by Rocket Doctor
As you probably know, NASA had one billion dollars to give out in contracts. Space X received $440 million of that.

Boeing and one othere company that i never heard of before divided up the remaining funds.

What did ATK Liberty get from that "pie" NOTHING !


They got nothing because they have only a paper launcher.
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  #18  
Old 08-17-2012, 01:55 PM
Rocket Doctor Rocket Doctor is offline
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Does Sierra Nevada corp and Boeing have launchers?
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  #19  
Old 08-17-2012, 02:57 PM
Jerry Irvine's Avatar
Jerry Irvine Jerry Irvine is offline
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Boeing has launchers. Pretty sure most them are either classified or partnering with other large firms. One guy who I know went to work for Marquardt, which was taken over by Hughes that division of which was taken over by Boing.

Boing has its fingers in everything.

http://www.boeing.com/defense-space/space/delta/

http://www.boeing.com/history/boeing/saturn.html

http://www.defenseworld.net/go/defe...ment%20Contract

http://online.wsj.com/article/SB100...3415041686.html

X-Cor was our neighbor at Mojave Airport where we did some very large solids firings.


9" x 144" solid 13,000 lb thrust a few feet from our building. Stick that in your Alpha and launch it. . .

Sierra Nevada is a proposal farm, and they have gotten a few hits lately, however the delivered results have been slim at best.

Last edited by Jerry Irvine : 08-17-2012 at 03:56 PM.
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  #20  
Old 08-17-2012, 04:25 PM
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luke strawwalker luke strawwalker is offline
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Quote:
Originally Posted by Jerry Irvine
Lookie.


What's you're point?? Those are LIQUID ROCKETS, which are perfectly capable of being move HORIZONTALLY, because they're moved EMPTY of propellants... SRB's on the other hand, must by their very nature, be moved FULLY FUELED with propellants and thus weighing millions of pound during transport... building something to carry them, let alone erect them, is a HUGE undertaking... doubt it, read the "summaries" on the 260 inch solid handling study that I posted over in the Scale section... massive barges, enormous lifting cradles, multiple pumpdowns and barge lifts in stages to get the blasted thing upright and on the pad... all of which means HUGE operations expenses...

Even the Soviet "Buran" shuttle was moved horizontally, because it used LIQUID rocket boosters that were moved to the pad EMPTY, and thus weighed very little compared to the American Shuttle stack with it's massive segmented SRB's. Horizontal moving and integration has proven itself cheaper than vertical integration, which is why most of the modern rockets have adopted that operations scheme... BUT, then again, they're all LIQUID vehicles with, at most small Solid booster motors strapped on the sides, NOT massive solid first stages...

Thanks for proving my point for me... Later! OL JR
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