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#540
by
Chris Bergin
on 18 Dec, 2014 03:22
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Sounds like what they know went well!
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#541
by
vyoma
on 18 Dec, 2014 03:23
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S200 and L110 performance were as expected. Unmanned crew module re-entry worked extremely well. Splashdown in Bay of Bengal.
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#542
by
Steven Pietrobon
on 18 Dec, 2014 03:23
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All stages performed well.
Crew module has splashed down in Bay of Bengal.
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#543
by
vyoma
on 18 Dec, 2014 03:25
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Announcement regarding LVM3 D1 (first developmental flight) to be expected in next 2 days.
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#544
by
Chris Bergin
on 18 Dec, 2014 03:25
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"We have a new launch vehicles" - holds the model.
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#545
by
vyoma
on 18 Dec, 2014 03:25
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"India, you have a new launch vehicle"
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#546
by
Steven Pietrobon
on 18 Dec, 2014 03:26
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India you have a new launch vehicle.
First development flight in two years. We call it LVM-3.
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#547
by
vyoma
on 18 Dec, 2014 03:27
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Control changeover from S200 to L110 was very good. S200 separation is novel too, uses 12 solid motors for graceful separation.
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#548
by
Prober
on 18 Dec, 2014 03:27
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#549
by
Steven Pietrobon
on 18 Dec, 2014 03:27
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First transition from solid to liquid.
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#550
by
ss1_3
on 18 Dec, 2014 03:28
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There have a separation video as well!
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#551
by
vyoma
on 18 Dec, 2014 03:29
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"Each S200 and L110 have performed to the dot" - Vehicle Director.
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#552
by
Steven Pietrobon
on 18 Dec, 2014 03:29
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Vehicle director. Performed to the dot.
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#553
by
Steven Pietrobon
on 18 Dec, 2014 03:30
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Associate vehicle director.
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#554
by
Steven Pietrobon
on 18 Dec, 2014 03:30
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Talking about module descent.
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#555
by
Steven Pietrobon
on 18 Dec, 2014 03:31
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Lost data 2 km altitude. Recovery crew on the way.
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#556
by
Steven Pietrobon
on 18 Dec, 2014 03:32
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Spent a lot of time looking at configurations for this vehicle.
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#557
by
Steven Pietrobon
on 18 Dec, 2014 03:34
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Introducing project director.
Go through tremendous amount of analysis.
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#558
by
vyoma
on 18 Dec, 2014 03:35
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Crew module performed as expected. Till 80km the control was ON and capsule was kept at right orientation. During re-entry crew module velocity was reduced from 5.3km/s to 230m/s and at 15 km altitude apex covers separated and pilot chute deployed (2.5m diameter). Later main chute deployed (31m diameter) and velocity reduced to 50m/s. Telemetry data was not received when altitude was less than 2km. Later telemetry acquired at splashdown via beacon. It is being recovered and brought to SDSC SHAR later.
"Fly an experiment on an experiment" - Crew Module mission director
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#559
by
Steven Pietrobon
on 18 Dec, 2014 03:36
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Great landmark in development of GSLV Mk.III vehicle.
