NASA NASA's X-43A Proves Hypersonic Scramjet Flight

  • Thread starter Thread starter Chen
  • Start date Start date
  • Tags Tags
    Flight
AI Thread Summary
NASA's X-43A has demonstrated the potential of hypersonic scramjet flight, achieving speeds up to Mach 10. While the scramjet engine is effective for atmospheric flight, it cannot operate in the vacuum of space, necessitating the use of rocket engines for missions beyond Earth's atmosphere. The technology could significantly reduce costs for launching satellites and components for lunar or Martian missions. Additionally, there are implications for ultra-fast shipping and advanced weapon systems due to the high speeds achievable. Overall, the advancements in scramjet technology mark a significant step toward future aerospace innovations.
Chen
Messages
976
Reaction score
1
http://www.sciencedaily.com/releases/2004/03/040329074842.htm

Sounds pretty neat, but I'm wondering what NASA is going to do with an oxygen-based scramjet engine. http://www.thedailyfarce.com/science.cfm?story=2004%5C03%5Cscience_x43aflies7timesspeedofsound_03200400054 it says "If we can get up to 10 times the speed of sound, man, we could probably get another $10 Billion from President Bush. He loves fast machines. I'll probably tell him that we can use the X-43A to go to the Moon or Mars. He'll love that." But how can this engine be used to go the Moon if there is no air along the way?!

(It took a lot of inner strength to ignore the humor in the quote by the way... I'd like to keep this on topic. :wink:)
 
Last edited by a moderator:
Physics news on Phys.org
The engine that took the Appollo missions to the moon did not burn most of the way there. These missions were accomplished by one big push at the beginning, then a lot of coasting. Most of the fuel burned on these missions was burned getting off the ground and up out of the atmosphere, while accelerating up to orbital speeds.The X-34 (well, actually, one of its larger decendants) can get this job done far more cheaply. After Mach 10 is achieved and the craft has left the atmosphere, rocket engines can do the rest.

With very little rocket boost, the hypersoar could be a spaceshuttle, or with even less rocket power (launched from a payload bay), it could be a very cheap method for delivering sattelites into orbit. Of course, this latter technique can also be used to put components for a Moon launch, or even a Mars launch into orbit, which is a much cheaper start-point from which to launch these missions.
 
Ok, I understood that much. But how will they take off from Mars or the Moon with these engines? There is no air over there, is there?
 
No,

A rocket of some sort will be needed in that case.

The scramjets aren't going to be enough on their own to get to orbit, but they can still provide the majority of the velocity. Every kg of oxidizer you pull from the air instead of bringing it along for the ride is more mass you can get to orbit.

More feasible offshoots of the research will be ultra-high fast shipments (when it absolutely, positively, has to be there yesterday...) or weapon systems (why use stealth when you're going so fast they can barely see you, let alone hit you).
 
enigma said:
ultra-high fast shipments (when it absolutely, positively, has to be there yesterday...)

:biggrin:

I have been hearing promises of the day that I can fly to China for lunch for most of my life; not that I could ever afford it mind you. This is the first real indicator that I have seen that such a thing might happen anytime soon - say in the next 20 or 30 years.

I predict that space elevators will eventually make this all a moot point for getting to space. It seems to me that the economy of elevators must win out once the technology becomes possible...which some claim is now.

Anyway, this is really, really cool. It's about time. :smile:
 
Ivan Seeking said:
Anyway, this is really, really cool. It's about time. :smile:
My thoughts exactly. I remember reading about this stuff like 15 years ago.
 
Venus does not have a magnetosphere, so the Galactic Cosmic Rays (GCRs) environment shall be much worse than in a LEO environment. Looking to the std radiation models for Venus, the standard radiation-hard space level electronic component with tested immunity LET = 85 MeV-cm2/mg seems not enough, so, for example, a 1cm2 Si die will suffer considerable flux above this level during a long mission (10 years for example). So, the question is, usually we are not paying attention to latch-up...
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
Back
Top