Space Stuff and Launch Info

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Discussion Overview

This thread discusses various recent developments and information in the field of aerospace, including upcoming launches, scientific missions, and discoveries related to space exploration. The scope includes theoretical insights, technical details, and observational data from missions such as SpaceX Dragon, NASA's Juno, and others.

Discussion Character

  • Exploratory
  • Technical explanation
  • Conceptual clarification
  • Debate/contested
  • Experimental/applied

Main Points Raised

  • Some participants share links to upcoming SpaceX launches and express interest in following the events.
  • There is mention of a digital tape recovered from the Columbia crash that contains footage of reentry plasma flashes, with requests for information on where to view it.
  • Discussion includes a write-up on the K2 mission and its discoveries regarding exoplanets.
  • Participants highlight the significance of NASA's Juno mission to Jupiter, which aims to study the Great Red Spot and its heat dynamics.
  • There is mention of an anomaly in star formation related to the object CX330, which is located in a star-forming region but lacks the typical surrounding gas and dust.
  • Some participants express optimism about government cooperation with private industries in advancing space technology.
  • Information is shared regarding Io's fluctuating atmosphere and the TESS mission's goals in exoplanet exploration.

Areas of Agreement / Disagreement

Participants express a range of views on the significance of recent developments, with some showing enthusiasm for collaborative efforts in space exploration while others raise questions about specific scientific phenomena. No consensus is reached on the implications of the discussed topics.

Contextual Notes

Some discussions involve complex scientific theories and observations that may depend on specific definitions or assumptions, which remain unresolved. The implications of certain findings are also not fully explored.

Who May Find This Useful

Readers interested in aerospace developments, space missions, and the latest scientific discoveries in astrophysics and planetary science may find this discussion valuable.

  • #781
Leveling off at 46,000 feet before launch...
 
Physics news on Phys.org
  • #782
six minutes now
 
  • #783
Safe landing. Great. :smile:
 
  • #784
Did anyone notice that the spaceplane doesn't seem to have a front wheel? They appear to use something more like a skid plate. My first thought was it reduces weight.
 
  • #785
Yeah, I guess they have to use the rear wheel brakes to control the low-speed steering?
 
  • #786
berkeman said:
Yeah, I guess they have to use the rear wheel brakes to control the low-speed steering?

Apparently so. But if you don't really need it, why build it? They only need steering for 30 seconds or so. I think beyond that it could all be done with air surfaces.
 
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  • #787
Heh, they might also be using the skid pad as an additional brake.
 
  • #788
Are there any replay videos of this flight? I some how missed it.
 
  • #789
dlgoff said:
Are there any replay videos of this flight? I some how missed it.
Post #780
 
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  • #790
Motore said:
Post #780
Yes, I watched that, but that's not a replay video.
 
  • #791
Motore said:
Post #780
Okay, I guess that does show what happened.
 
  • #792
dlgoff said:
Yes, I watched that, but that's not a replay video.
Did anone else feel this was closer to Evel Knievel at the Snake River than Yuri or Alan?? Maybe that's the point, but it all seemed just a little "off" to me...I guess I,m showing my age.
 
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  • #793
Well, thankfully this mission was more successful than that failed "jump" by Evel.
 
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  • #794
hutchphd said:
Did anone else feel this was closer to Evel Knievel at the Snake River than Yuri or Alan?? Maybe that's the point, but it all seemed just a little "off" to me...I guess I,m showing my age.

Haha, I know what you mean. But this isn't Evel Knievel. These guys are doing it right. I think the biggest notable differences between this and a NASA operation are the reduced scale, and they are only providing what amounts to a thrill ride.
 
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  • #795
Does anybody know what the contingencies are for failed mission landings? Are there other airstrips in the area that can be used as alternates for glided landings? How long of an airstrip does the lander need? Does the craft have the capability to dump its rocket fuel if needed to lighten before an emergency landing?
 
  • #796
What would be the scenario where they need to go to a different landing site farther away? Release is just ~15 min before landing, so they can make sure the weather conditions will be fine.

I liked the coverage, just the constant comparisons to Apollo 11 were annoying. This was not another Moon landing event. Not even close.
 
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  • #797
berkeman said:
Does anybody know what the contingencies are for failed mission landings? Are there other airstrips in the area that can be used as alternates for glided landings? How long of an airstrip does the lander need? Does the craft have the capability to dump its rocket fuel if needed to lighten before an emergency landing?
In October 2010, the 3,000 m (10,000 ft) runway at Spaceport America was opened, with SpaceShipTwo "VSS Enterprise" shipped to the site carried underneath the fuselage of Virgin Galactic's Mother Ship Eve.

compliments of this google search:
https://www.google.com/search?q=vir...AEAoAEBqgEHZ3dzLXdpesgBCMABAQ&sclient=gws-wiz

I guess this came from this Wikipedia page:
https://en.wikipedia.org/wiki/Virgin_Galactic
 
  • #798
hutchphd said:
Did anone else feel this was closer to Evel Knievel at the Snake River than Yuri or Alan?? Maybe that's the point, but it all seemed just a little "off" to me...I guess I,m showing my age.

The only point of this stunt was to sell space tickets. It's just a show. People already go to space on a regular basis.
 
  • #799
  • #800
Office_Shredder said:
The only point of this stunt was to sell space tickets. It's just a show. People already go to space on a regular basis.
True, but I think we have to give the guy credit for risking his own life to help make that happen.
 
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  • #801
berkeman said:
True, but I think we have to give the guy credit for risking his own life to help make that happen.

To be clear, I am not opposed to stunts. Virgin galactic was a huge struggle for him to get operational, and if he wants to throw himself a party more power to him.
 
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  • #802
berkeman said:
True, but I think we have to give the guy credit for risking his own life to help make that happen.
It takes many steps to create and fund a safe industry. I don't think height is the long term aim. Height is a step needed for funding, by flying the affluent early passengers.
It will all change again when one can buy an orbital flight.
 
  • #803
You can buy orbital flights.
Axiom sells Crew Dragon seats to fly to the ISS for $55 million each. First flight early 2022. You can also buy a full Crew Dragon flight. Inspiration4 in two months will be the first of these flights.
 
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  • #804
DearMoon application sneak peek
One million applications for 8 seats - not even NASA's astronaut selection is that selective. No decision yet, but presumably the candidates featured in that video are still in the race.

----

More mystery around the upcoming Blue Origin flight (July 20). The original winner moved to a later flight, citing unspecified "scheduling concerns". What unexpected event could make you miss that opportunity? Combined with no announcement of who won, people wonder if someone didn't want the publicity. But then... why did they bid in the first place? It was obviously going to be a big media event.

Now the seat went to Oliver Daemen, son of a Dutch investment banker. The two Bezos brothers fly, and they invited Wally Funk, who likely would have been an astronaut in the 1960s if NASA would have allowed women to fly at that time. The flight will set new records for both the youngest (18) and oldest (82) person in space.

----

July 21 the Nauka module will be launched to the ISS, one of its last big components. It also comes with the European Robot Arm, which will help on the Russian side of the ISS.

July 30 Boeing will repeat the uncrewed flight test of Starliner.
 
  • #806
It is interesting that there are now two completely different sub-orbital spaceflight experiences available to the public. Both are based on approaches to space taken over fifty years ago with some modern upgrades. I don't know if the public realizes that some of the X-15 flights actually reached space and thus those pilots were really the first American astronauts. Also, Neil Armstrong was an X-15 pilot.
 
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  • #807
Does anyone know how much hydrogen the Blue Origin flight required? I haven't found any references to the tank sizes, consumption, or anything other than a lot of attention to it not using a carbon fuel. But of course, most hydrogen is produced from hydrocarbons. I've found some numbers for the conversion factors, but I still haven't found the amount of hydrogen consumed.

Mods - if this should be it's own topic, I'll delete and move it.
 
  • #808
BE-3 has a maximal thrust of 490 kN and a burn time of 140 s, and while I don't find the I_sp it should be somewhere in the 350-450 range as it ascends through the atmosphere. With the worst case assumption it would consume 490 kN * 140s / (3500 m/s) = 20 t of fuel, out of that ~2 tonnes of hydrogen. In practice the engine might throttle down as the rocket gets lighter, and its I_sp gets better, so it might only need 1.5 tonnes or so.
 
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  • #809
For example, space company SpaceX has set itself the goal of colonizing Mars for the continued existence of mankind. Associated not only with Elon's dream, but also with the small reserves of the Earth. Perhaps our children will be able to see the Earth from Mars in a couple of ten years.
 
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  • #810
mfb said:
BE-3 has a maximal thrust of 490 kN and a burn time of 140 s, and while I don't find the I_sp it should be somewhere in the 350-450 range as it ascends through the atmosphere. With the worst case assumption it would consume 490 kN * 140s / (3500 m/s) = 20 t of fuel, out of that ~2 tonnes of hydrogen. In practice the engine might throttle down as the rocket gets lighter, and its I_sp gets better, so it might only need 1.5 tonnes or so.
Thanks. This being a physics forum, I was thinking someone might estimate the amount by calculating mass, time, and required thrust. I was surpised I couldn't just find a number, given all the space geeks out there. I'll do some calcs later using your estimate.
 

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