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Questions tagged [atlas-v]

Atlas V is an expendable launch system in the Atlas rocket family.

7 votes
1 answer
2k views

Did the Starliner perform an inflight abort test? I could not find any videos to support the same. Isn't a pad abort and an in flight abort neccesary before sending humans to space? Can the starliner'...
Ashvin's user avatar
  • 3,440
3 votes
0 answers
179 views

I was tasked with researching certain properties of the RD-180 engine. I am finding contradictory information, or I am unable to find it at all. I am looking for the following information Mixture ...
PilotGeometer's user avatar
12 votes
1 answer
1k views

In Boeing's OFT-2 mission, an Atlas V is the launch vehicle. The solid rocket booster burns out at T+ 1:35 minutes, but the boosters are jettisoned at T+ 2:40 minutes. Why are the boosters not ...
Ashvin's user avatar
  • 3,440
2 votes
0 answers
102 views

In the livestream of the latest Atlas V 541 flight launching the GOES-T satelite I saw that the nosecones of the two visible boosters changed the appearance within a few seconds in the flight. Is this ...
Spaceman-21's user avatar
6 votes
1 answer
398 views

I've never noticed this before, so I'm asking. Shortly after SRB ejection, the RD-180 plume appears to be very asymmetric. Why is this? If I recall correctly, these are full-flow & there isn't any ...
Anton Hengst's user avatar
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3 votes
0 answers
98 views

We all know and mourn that the Atlas V will never fly in a three-core configuration. What, if anything, prevents me from legally purchasing three CCBs and launching my own Atlas V Heavy, provided I ...
Anton Hengst's user avatar
  • 11.8k
3 votes
1 answer
237 views

RUAG Space is the company that manufactures payload fairings for the Ariane, Vega, Atlas V (500 series) and the upcoming Vulcan. Back when Spacex started trying to catch the fairing without it hitting ...
Speedphoenix's user avatar
  • 5,545
8 votes
0 answers
99 views

When centaur separates the payload, we can see a video signal of this happening. The mission of centaur is completed now, but are there still some activities centaur is performing after seperation? ...
RAD6000's user avatar
  • 1,264
4 votes
0 answers
88 views

The Wikipedia page on the GEM-63 says that the Atlas V will start using it "in July 2019." But the Atlas V page says that the switch from the AJ-60A will happen "in the near future." That the switch ...
A. Howells's user avatar
3 votes
0 answers
203 views

According to NASA's blog, one of the problems with the failed Starliner mission was An error with the Mission Elapsed Timer (MET), which incorrectly polled time from the Atlas V booster nearly 11 ...
Machavity's user avatar
  • 8,236
4 votes
0 answers
179 views

All sources that I can find indicate that they are isogrid (or possibly orthogrid?) structural tanks manufactured of milled aluminum. However, I cannot find further detail about of which alloy ...
Anton Hengst's user avatar
  • 11.8k
2 votes
0 answers
148 views

Is safe booster separation (they call it "jettison") without recontact assured by separation motors, pushers, or what? The Juno Mission Overview refers to "structural thrusters" but that means ...
Organic Marble's user avatar
2 votes
0 answers
102 views

I was looking at the Juno space probe which was launched in August 2011 onboard an Atlas V 551. In particular I was looking at https://elvperf.ksc.nasa.gov/Pages/News.aspx and using the performance ...
chuckstables's user avatar
14 votes
1 answer
3k views

When including an image in an answer to this question: Was New Horizons launched on a copper rocket? I noticed that for the larger diameter fairings (Atlas 501 and up) the Centaur upper stage is ...
Organic Marble's user avatar
2 votes
1 answer
381 views

I can't find this information anywhere for the single or double engine variant. could it be variable? Or is it a secret?
sleepingNewton's user avatar

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