Updates Blue Origin New Shepard News and Updates

indy91

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Hire Russians. "Launch. Everything Nominal. Nominal. Everything Nominal. Stage 1 separation nominal. Nominal" :)

Russians? What about Nominal, ehm, Orbital Sciences?

 

Fabri91

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New newsletter:
Our next flight is going to be dramatic, no matter how it ends.

Like Mercury, Apollo, and Soyuz, New Shepard has an escape system that can quickly propel the crew capsule to safety if a problem is detected with the booster. Our escape system, however, is configured differently from those earlier designs. They mounted the escape motor on a tower above the capsule – a “tractor” configuration – the escape motor would pull the capsule away from a failing booster. But because a capsule cannot reenter Earth’s atmosphere or deploy parachutes with a tower on top, the tower, along with the escape motor, must be jettisoned on every flight – even the nominal flights. Expending an escape motor on every flight drives up costs significantly. Further, the jettison operation is itself safety critical. Failure to jettison the tower is catastrophic.

The New Shepard escape motor pushes rather than pulls and is mounted underneath the capsule rather than on a tower. There is no jettison operation. On a nominal mission, the escape motor is not expended and can be flown again and again. We’ve already tested our pusher escape system, including many ground tests and a successful pad escape test, but this upcoming flight will be our toughest test yet. We’ll intentionally trigger an escape in flight and at the most stressing condition: maximum dynamic pressure through transonic velocities.

Capsule in-flight escape testing was last done during the Apollo program. From 1964-1966, in-flight escape tests were performed with Apollo simulator capsules using an expendable booster called the Little Joe II. We’ll be doing our in-flight escape test with the same reusable New Shepard booster that we’ve already flown four times. About 45 seconds after liftoff at about 16,000 feet, we’ll intentionally command escape. Redundant separation systems will sever the crew capsule from the booster at the same time we ignite the escape motor. You can get an idea of what will happen in this animation. The escape motor will vector thrust to steer the capsule to the side, out of the booster’s path. The high acceleration portion of the escape lasts less than two seconds, but by then the capsule will be hundreds of feet away and diverging quickly. It will traverse twice through transonic velocities – the most difficult control region – during the acceleration burn and subsequent deceleration. The capsule will then coast, stabilized by reaction control thrusters, until it starts descending. Its three drogue parachutes will deploy near the top of its flight path, followed shortly thereafter by main parachutes.

What of the booster? It’s the first ever rocket booster to fly above the Karman line into space and then land vertically upon the Earth. And it’s done so multiple times. We’d really like to retire it after this test and put it in a museum. Sadly, that’s not likely. This test will probably destroy the booster. The booster was never designed to survive an in-flight escape. The capsule escape motor will slam the booster with 70,000 pounds of off-axis force delivered by searing hot exhaust. The aerodynamic shape of the vehicle quickly changes from leading with the capsule to leading with the ring fin, and this all happens at maximum dynamic pressure. Nevertheless, the booster is very robust and our Monte Carlo simulations show there’s some chance we can fly through these disturbances and recover the booster. If the booster does manage to survive this flight – its fifth – we will in fact reward it for its service with a retirement party and put it in a museum. In the more likely event that we end up sacrificing the booster in service of this test, it will still have most of its propellant on board at the time escape is triggered, and its impact with the desert floor will be most impressive.

The test should be in the first part of October, and we’ll webcast it live for your viewing pleasure. Details to come.

If someone forwarded this email to you and you’d like to subscribe to get these updates yourself, you can do so here. In my next email update, I hope to give you a sneak peek of the orbital vehicle we’ve been working on for the last few years.

Gradatim Ferociter!

Jeff Bezos

(Added emphasis is mine)
 

IronRain

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In the more likely event that we end up sacrificing the booster in service of this test, it will still have most of its propellant on board at the time escape is triggered, and its impact with the desert floor will be most impressive.

The test should be in the first part of October, and we’ll webcast it live for your viewing pleasure. Details to come.

I like the way this article is written. No sorrow for destroying the booster; it's going to be a hell of a show!
 

GLS

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I like the way this article is written. No sorrow for destroying the booster; it's going to be a hell of a show!

It will be cool, but not this cool... :cool:


It will similar to this:
(can't find the angle showing the Atlas blowing up after the abort :()
 

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The planning application for the Blue orbital launch site is now online, and provides us with a few details on the Orbital LV and it's operations (mostly in 'Drainage Analysis Technical Memorandum' under 'application'). Probably most notable is that first stages are to be recovered on an 'ocean-going platform', about 750 nautical miles offshore. That's a lot farther out than in SpaceX's version of the concept; and implies either it's a big vehicle with more overall Delta-V, or that they're skewing LV proportion towards the booster to save on expendable upper stages.

Presumably this is why Bezos is giving his 'sneak peek' of the system now; we're at the point where info will get out, whether he wants it to or not.
 

GLS

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Just a heads-up, the launch (abort) is tomorrow with webcast starting at 1050AM ET.
 

Urwumpe

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Just a heads-up, the launch (abort) is tomorrow with webcast starting at 1050AM ET.

So, should I have an early end of work, I could watch it...
 

MaverickSawyer

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So, should I have an early end of work, I could watch it...

Might want to scrub the viewing party tomorrow and wait a day:

[ame="http://twitter.com/blueorigin/status/783023859473657856"]Blue Origin on Twitter: "Weather no-go for tomorrow’s New Shepard #InFlightEscape test. Webcast now Wednesday 10:45 am ET. #GradatimFerociter"[/ame]
 

Urwumpe

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No problem, I have an exceptionally calm week ahead. :lol:
 

Nicholas Kang

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Blue Origin official live webcast will begin at T-15.



---------- Post added at 10:45 PM ---------- Previous post was at 10:32 PM ----------

Official webcast has begun!

---------- Post added at 10:50 PM ---------- Previous post was at 10:45 PM ----------

T-10 minutes and counting.

---------- Post added at 10:55 PM ---------- Previous post was at 10:50 PM ----------

T-5 minutes and counting.
 
Last edited:

GLS

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I'll be laughing until next year if the capsule separates and the booster continues into space and then land as usual. :rofl:
 

Nicholas Kang

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Booster to internal power.
 

GLS

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Nicholas Kang

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Short hold at T-2 minutes and 11 seconds.
 

GLS

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and counting again....

---------- Post added at 04:00 PM ---------- Previous post was at 03:59 PM ----------

another hold

---------- Post added at 04:02 PM ---------- Previous post was at 04:00 PM ----------

Countdown holding for 3 minutes now.

---------- Post added at 04:07 PM ---------- Previous post was at 04:02 PM ----------

Hold is now 7 minutes long...
 

Urwumpe

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Did they just turn off the APU?

Sounds like a problem in Texas.
 

Donamy

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Corn Ranch, we have problem.
 

GLS

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There was some issue with the booster, waiting for assessment on whether to proceed or scrub.

---------- Post added at 04:20 PM ---------- Previous post was at 04:16 PM ----------

Assessing for 20 minutes now.

---------- Post added at 04:21 PM ---------- Previous post was at 04:20 PM ----------

T-15 and counting now!

---------- Post added at 04:22 PM ---------- Previous post was at 04:21 PM ----------

T-13 minutes and counting.

---------- Post added at 04:29 PM ---------- Previous post was at 04:22 PM ----------

T-6 minutes and (still) counting.

---------- Post added at 04:32 PM ---------- Previous post was at 04:29 PM ----------

T-200 seconds.

---------- Post added at 04:33 PM ---------- Previous post was at 04:32 PM ----------

T-100 seconds

---------- Post added at 04:34 PM ---------- Previous post was at 04:33 PM ----------

hold again

---------- Post added at 04:35 PM ---------- Previous post was at 04:34 PM ----------

counting again!
T-1:20

---------- Post added at 04:36 PM ---------- Previous post was at 04:35 PM ----------

T-30 seconds!
 
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