Author Topic: FAILURE: OS-M1 maiden flight - Lingque-1B - Jiuquan - March 27, 2019 (09:39 UTC)  (Read 27323 times)

Offline Galactic Penguin SST

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Offline GELORD

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Offline Steven Pietrobon

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Those photos look pretty convincing. The exhaust trail for the second stage cuts off not long after first stage separation, seen in the gap between the trails. They should have followed what Rocketlab did with their first launch, flying a dummy satellite which was not worth much. Feel sorry for the people who built the payload.
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Offline SmallKing

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Offline Phillip Clark

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Where will launch a rocket? Who knows?

The launch pads are shown as TLE-1 and TLE-2.   I thought that one of these areas had been identified as being 43-95?   If correct, is #2 = 43-95?

The ZQ-1 launch site was referred to as being "E2" so perhaps it was "TLE-2"?
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Offline Kosmos2001

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It looks like a missile launch with those sudden turns.

Online Chris Bergin

Was hoping we'd have an official statement by now, but anyway, sad news.

Rui's article:

https://www.nasaspaceflight.com/2019/03/maiden-launch-of-onespace-os-m-rocket-fails/
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Offline Galactic Penguin SST

Was hoping we'd have an official statement by now, but anyway, sad news.

Rui's article:

https://www.nasaspaceflight.com/2019/03/maiden-launch-of-onespace-os-m-rocket-fails/

Chinese media quoted OneSpace that they will issue an official statement later.
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Offline anik

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Where will launch a rocket? Who knows?

It seems that the same launch pad as for ZQ-1.

Offline PM3

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« Last Edit: 03/27/2019 02:09 pm by PM3 »
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Available info says the launch was at 0939UTC.

Offline Galactic Penguin SST

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Online edkyle99

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At least one prelaunch image shows a vehicle, perhaps a prototype, with a finned second stage that looks almost identical to the first stage.  Most other photos show no fins on the second stage.  These appear to be short range missile motors fitted with steering vanes and fins that were originally designed to work in the lower atmosphere.  Likely a tough flight control problem to solve for second stage flight if the fins are removed, and probably not easy if the fins are retained.  Scout, for example, had to have a gas jet control system for its second stage.

 - Ed Kyle
« Last Edit: 03/29/2019 12:09 pm by edkyle99 »

Offline Galactic Penguin SST

Finally an official statement: https://mp.weixin.qq.com/s/Yx6OWZgz77X6HV7CK89aAg

"Preliminary investigation shows that a malfunction of the velocity gyroscope at T+45.68 seconds lead to loss of attitude control."
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Offline Olaf

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Offline eeergo

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