You wrote: "You'll find that the detonation velocity for hydrogen-air at STP is 1968 m/sec"

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You wrote: "You'll find that the detonation velocity for hydrogen-air at STP is 1968 m/sec"

David F Mayer — 6/2/2004 7:06:04 AM (archived)

But, conditions in the combustor will be much different.

Air will be adiabatically heated by compression be several hundred degrees C. This does several things, including greatly increasing the detonation velocity.

Next, it is possible to have a continuous ignition energy applied to the mixture by microwaves. These will produce a glow discharge which will generate lots of hydrogen atoms, which react very rapidly with oxygen in air.

Mixing of hydrogen with air seems to be a problem, but it may be amenable of solution as well.

David F Mayer

The whole thread (31 posts)

Airships to orbit - Tom Brosz - 5/27/2004 3:07:34 AM
- re: I don't understand why anyone would build all that hardware if they didn't do the numbers - Success_Machine - 5/31/2004 4:10:21 PM
  - There's no way you'll get an L/D of 50 - Gary - 5/31/2004 8:27:13 PM
    - re: I believe it does get an L/D of 50, when forced to go hypersonic speed - Success_Machine - 6/1/2004 11:06:48 AM
- There are exactly TWO practical ways of launching a payload into orbit. - David F Mayer - 5/30/2004 5:22:24 AM
  - Actually...... - Gary - 5/31/2004 8:31:49 PM
    - A scramjet won't get you into orbit (they flame out at Mach 10). - David F Mayer - 6/1/2004 1:03:18 AM
      - Scramjet 101 - Gary - 6/1/2004 4:35:26 AM
        
        re: Scramjet 101 - David F Mayer - 6/2/2004 12:32:24 AM
        
        Use a detonation wave analogy to understand this - Gary - 6/2/2004 3:27:55 AM
        
        You wrote: "You'll find that the detonation velocity for hydrogen-air at STP is 1968 m/sec" - David F Mayer - 6/2/2004 7:06:04 AM
        
        Yes, air for combustion is pre-heated by the bow shock - Gary - 6/2/2004 4:25:13 PM
        
        re: The only design for a scramjet that works in theory - Success_Machine - 6/2/2004 1:09:56 PM
        
        re: Controlled Flame Speed Limited to Mach 5 - Success_Machine - 6/2/2004 2:34:40 AM
- Do the numbers, Tom. Then forget it. - David F Mayer - 5/30/2004 5:09:45 AM
  - re: Do the numbers - Tom Brosz - 5/30/2004 6:22:58 AM
    - Look at the VOLUME of a balloon of ANY type required to lift a reasonable spacecraft to 30,000 meters. - David F Mayer - 5/30/2004 1:35:00 PM
  - I was only referring to using a balloon to lift a rocket here. (n/t) - DFM - 5/30/2004 5:19:50 AM
- re: Airships to orbit - Nathan Koren - 5/28/2004 3:12:12 AM
- It was me... - Adam - 5/27/2004 11:33:12 AM
- Low thrust to orbit for an airship has got to be bogus - Gary - 5/27/2004 5:52:06 AM
  - "Something is not right here." You are correct. The concept is bullshit! (n/t) - David F Mayer - 5/30/2004 5:17:07 AM
  - Color me skeptical - Larry J - 5/27/2004 6:12:43 PM
    - power sources... - Adam - 6/1/2004 11:19:27 PM
      - Still very skeptical - Larry J - 6/2/2004 2:33:32 PM
    - re: Skipping Over the Atmosphere on a Surfboard - Success_Machine - 5/27/2004 9:04:04 PM
  - re: Low thrust to orbit for an airship has got to be bogus - Adam - 5/27/2004 11:31:06 AM
    - Use VASIMR - phil - 5/27/2004 12:42:19 PM
      - For a large balloon, at any altitude, the air resistance even at low speed is comparable to its weight. I STILL say the idea is bullshit. (n/t) - David F Mayer - 5/30/2004 1:37:21 PM
- re: Airships to orbit - Raoul - 5/27/2004 5:35:39 AM
  - Visible Horizon... - Adam - 5/27/2004 11:30:18 AM

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