Novel take-off & landing device
Novel take-off & landing device
Author: Judbarovski David, systems
engineering, principle inventor
The Article is not correct, because supercritical regions of gases at 1300 atm
Abstract
The take-off & landing device is four
special water jets. The water is thrust out through a nozzle by gases at high
pressure after ignition of “unitary liquid combustible” (ULC), i.e. stoichiometric
composition of ammonium nitrate with urea, and liquefied by water as a solvent.
Take-off and then lending of aircraft of 10.0
ton full weight consume about 2.0 m3 of water for the water jet and 235 kg of
ULC.
G = Q * t ; Q = F / v ; v^2 = 2 * g * 10 * P
Here G (kg) – water consume for take-off or
landing (1.0 m3)
Q (kg/s) – water consume (200 kg/s)
t (sec) – a time of take-off or landing (5.0
sec.)
F (Newton) – the water jets total thrust (near
10 ton)
v (m/s) – water outlet velocity through the
nozzle (550 m/s)
P (atm) – ULC gases pressure on the water
container (near 1300 atm)
g (m/s^2) – gravity acceleration (9.8
m/s)
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