(582B)
Flame-Front
Where it is first named
For example, Taper Resonant Cavity (590) of Figure (6-2) as to (820B) of Figure (8-6) is ideally suited for internal combustion I. C. engines as well as Rocket Engines where high thrust-yield of explosive power (gtnt) (582B) is required;
How it is written
- (582 A,B,C) 1× with (582) Flame-Front, (582A) Flame-Front, (582C) Flame-Front
- (582B) 1×
Drawings 5
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Figure (8-6) · 8-2 - Traveling Voltage Wave-Guides
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(820B) of Figure (8-6) · 8-7 - Application of Usage
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(820C) of Figure (8-6) · 8-7 - Application of Usage
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Figure (820A) of Figure (8-6) · 8-7 - Application of Usage
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The figure it sits on · WFC 427 Illustrations
Where it is named · 2
8-7 - Application of Usage 2×
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For example, Taper Resonant Cavity (590) of Figure (6-2) as to (820B) of Figure (8-6) is ideally suited for internal combustion I. C. engines as well as Rocket Engines where high thrust-yield of explosive power (gtnt) (582B) is required;
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Flame-Front (582 A,B,C)
In each and all Flame-Front (582 A,B,C) Resonant Pulse Waves are produced to net higher energy-yield beyond normal gas burning levels. Laser Energy (588) being injected into Resonant Pulse Waves (16) by way of Laser Inject Tube-Port (589) helps maintain Plasma-temperatures at extremely elevated temperatures over the prior art.
