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Blue Origin Thread (merged)


Aethon

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I have to admit I'm always somewhat excited by the looks of controlled fire. Any kind (well, probably apart from stove and refineries...)

Regarding launchers, the Vega IXV launch was so fast... Is it due to TWR ? SLT ? Is that save (I mean, can anyone give acceleration data ?)

The Vega is basically 3 SRB's on top of each other with a liquid engine for the final stage. Thing has a stupid high TWR, considering the cargo it was carrying.

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The seas were deemed too difficult to send out an uncrewed automated ship that survived a rocket crashing into it with barely a scratch.

I rather doubt there were any russian trawlers with dashcams nearby. :P

But the first stage had a camera on board, it could transmit the video in vhf or uhf.

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Chances are it won't be much different from the footage of the previous splashdowns.

Yeah, but something is better than nothing.

Some news (I guess) and details as maps about the landing pad agreement with US force.

http://www.patrick.af.mil/shared/media/document/AFD-141107-004.pdf

Gizmag source:

"SpaceX outlined its plans for the LC-13 pad, which will consist of a 750-ft (228-m) diameter pad of compressed soil and gravel designed to support the thrust and weight of returning spacecraft, and four 150-ft (45-m) contingency pads on the periphery for last-second emergency landings. In addition, SpaceX will build an access road and a mobile crane to move landed vehicles."

Edited by AngelLestat
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OK, thanks. I was under the impression that the Falcon's second stage put DSCOVR into its current 170 km x 1.37 million km transfer orbit and was therefore also in that orbit. I unferstood that DSCOVR's own thrusters would merely bump it from the transfer orbit into "orbit" around Earth-Sun L1.

PakledHostage, you are correct. The Falcon 9's second stage put DSCOVR into the 187x1.37m km orbit. (See SpaceX's press kit here, where you can see that they were targeting a very slightly lower apogee. The webcast on NasaTV also made it clear, that orbit was achieved after the second burn of the second stage, before the spacecraft separated from the stage.)

According to spaceflight101.com, DSCOVR carries enough fuel for about 600 m/s total delta-V. That's to last over its entire lifetime, so is mostly meant for stationkeeping; it's certainly not enough to get the spacecraft to L1 from anything but an orbit that already gets it very close.

Also, the second stage does achieve escape velocity, and in fact will be disposed of in solar orbit. (See SpaceX's filing with the FCC for the launch here, where they state "... launch vehicle Earth-escape second stage to be disposed of in Sun." "in Sun" is believed to be an error, where what they meant was solar orbit. The delta-V required to drop the stage's solar orbit's periapsis into the sun would be enormous.)

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The Vega is basically 3 SRB's on top of each other with a liquid engine for the final stage. Thing has a stupid high TWR, considering the cargo it was carrying.

Hmm... Maybe it's common for all SRB launch... Minotaur seems to also get fast quickly.

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The barge got pulled back into Jacksonville port yesterday, after having been conspicuously absent ever since the launch (even though the tug returned intermittently). People were speculating whether it might have been sunk, or at least severely damaged, by the storm...

Well, turns out, 8 meter high wave action is no joke even on a ship designed to handle almost anything.

http://imgur.com/EPLYgy8,A4FHWJO,vhJm1s5,bOBfpfT,pfJPbnd

Ouch.

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They're not being very lucky with this barge-landing thing. It's turning out to be much harder than anticipated.

Once they get the approvals, landing on solid ground is going to be a walk in the park compared to this.

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Didn't the first landing got the rocket bounced on one of them and demolish it?

Poor containers.

Yeah, it got shredded in half. Sacrifices must be made...

They're not being very lucky with this barge-landing thing. It's turning out to be much harder than anticipated.

Once they get the approvals, landing on solid ground is going to be a walk in the park compared to this.

I'm pretty sure that approval was recently given for construction of a launch pad for landing return stages at Kennedy. I think the current plan for the barge is to land the falcon heavy boosters? I forget if that was speculation or announced.

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I'm pretty sure that approval was recently given for construction of a launch pad for landing return stages at Kennedy.

Actually at Cape Canaveral; hence the need to wait for USAF approval, the cape being legally a USAF base.

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Looks like SpaceX is skipping a replacement for their F9R Dev 1 (the one that blew up last year). Deemed unnecessary as their current landing attempts provide all the data they need. The F9R Dev2 core may be used for the in-flight abort test of crew Dragon later this year -- perhaps even the Dragonfly. No more grasshopper program though.

Original with paywall: http://sen.com/blogs/irene-klotz/spacex-bypassing-replacement-for-lost-falcon-9r-landing-test-vehicle

Read the full article here: http://www.reddit.com/r/spacex/comments/2wgpyz/irene_klotz_on_twitter_spacex_skipping/coqnxtj

Last month, a Falcon 9 rocket came close to landing itself on a barge in the ocean, but it ran out of hydraulic fluid to maneuver its fins and crashed into the platform. A second attempt last week was stymied by high seas, but the rocket did successfully slow its descent and hover above the ocean’s surface before toppling over.

The ocean tests have been so successful that SpaceX is not currently planning to build a replacement for the Falcon 9R that was destroyed last year.

“We’re learning so much now, given the success of our returned vehicles, that when you can have full-envelope knowledge at a point that you’re only very closely missing the target then such an article doesn’t give you a great deal of additional learning,†Andy Lambert, SpaceX vice president of production, said in an interview.

That doesn’t mean SpaceX is abandoning Spaceport America. The company has invested more than $2 million in facilities, said spaceport director Christine Anderson.

“We’re hoping they’ll start up in the spring,†she said.

Instead of Falcon 9R demonstration vehicles, the company seems likely to use Spaceport America as a testing ground for boosters that manage to land intact, with the goal of learning how well the rockets hold up during reflight. SpaceX declined to comment.

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I think the current plan for the barge is to land the falcon heavy boosters? I forget if that was speculation or announced.

It is speculation, but recovering the boosters seems to fit with their business plan. There hasn't been an official announcement that I'm aware of.

What is worrying is that landing on a barge in the middle of the ocean appears to bring a whole new set of constraints (barge maintenance and availability, oceanic weather, etc...) which added to the launch constraints that are dictated by the payload (pad weather, launch windows, etc...), is going to make commercial offerings a bit awkward.

Speculations were that they would offer a discount for FH launches with recoverable boosters, but the recoverable booster option is not only going to have a much reduced payload, but is also going to have extra launch constraints tied to weather conditions at the recovery site and to the availability of the barge. Customers will have to accept a higher risk of scrubs and operational delays, which reduces the value of the reusable offering. Also increasing the possibility of recovery-related delays puts more pressure on SpaceX's already tight launch schedule. In the end, it might not all be worth it from a business perspective.

Edited by Nibb31
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Didn't the first landing got the rocket bounced on one of them and demolish it?

Poor containers.

This is why people want it renamed after a certian other Ian M Banks spaceship...

General Service Vehical "Only Slightly Bent"

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