Pre-recorded interview with Robin Fisher
Moonfacts for kids from NASA:
Square and Stationary Earth.
Theia’s mythological role as the mother of the Moon goddess Selene is alluded to in the application of the name to a HYPOTHETICAL planet which, according to the giant impact hypothesis, collided with the Earth, resulting in the Moon’s creation.
(Mysticism – Occult doctrine)
Journal of Geophysical Sciences, Solid Earth – Lunar and planetary Science Conference proceedings papers – 220;Moon to coalesce and reach hydrostatic equilibrium. between gravity and pressure, forming a spherical object. This has all been MATHEMATICALLY modeled.” – ” it’s core is “off center.”
Moon is a oblate spheroid.
– an ellipsoid with TWO EQUAL (opposing) semi-diameters.
If Apollo missions didn’t happen, as is almost impossible based on physics and research, then how does one account for Lunar Meteorites being testable or comparable to Moon rocks.
Moon rocks collected by astronauts during the Apollo program contain traces of apatite
The first form of elemental phosphorus to be produced (white phosphorus, in 1669) emits a faint glow upon exposure to oxygen – hence its name given from Greek mythology, meaning 220;light-bearer” (Latin Lucifer).
…did not diminish over time (and did not need re-exposure to light like the previously discovered… Brand at first tried to keep the method secret, but later sold the recipe for 200 thalers to D Krafft from Dresden, who could now make it as well, and toured much of Europe with it, including England, where he met with Robert Boyle.
Rosicrucian 18th Degree Freemason – Invisible College – Gresham College
Elemental phosphorus exists in two major forms—white phosphorus and red phosphorus
Google Glowing Phosphorus
If a rocket worked in space it only proves that there is an atmosphere in space which creates balance on the inner and outer parts of the space vessel.
The gasses are expanding rapidly out of one end of the rocket, but they are expanding into a vacuum, this vacuum is ‘sucking’ on the gasses as quick as they expand so the net result is zero force in one direction. Many people think that if oxygen and fuel is carried it makes a difference. But the principles of a vacuum does not cater for this man-made theory. All a vacuum wants is to be filled with something and anything. If some thing is expanding in a vacuum it will do so without any resistance because it has the aid of the vacuum itself.
In 1903, Konstantin Tsiolkovsky published (The Exploration of Cosmic Space by Means of Reaction Devices), the first serious scientific work on space travel. The Tsiolkovsky rocket equation—the principle that governs rocket propulsion. He also advocated the use of liquid hydrogen and oxygen for propellant, calculating their maximum exhaust velocity.
The delta-v needed to achieve low earth orbit starts around….
8 643 (m/s)
9.4km/s – 11.2 (33,840km/h – 40,000)
Max speed liquid oxygen/liquid hydrogen rockets (16,063km/h)
A typical value for the specific impulse of current rockets.
Propellant mix – liquid oxygen/liquid hydrogen
Vacuum Isp (seconds) – 455
Effective exhaust velocity (m/s) – 4462
As of 2013, the X-15 holds the official world record for the fastest speed ever reached by a manned aircraft. Its maximum speed was 4,520 miles per hour (7,274 km/h).
Speed of the Space Shuttle when the solid rocket boosters separate.
Operational altitude: 100 to 520 nmi (190 to 960 km; 120 to 600 mi)
Speed: 7,743 m/s (27,870 km/h; 17,320 mph)
Crossrange: 1,085 nmi (2,009 km; 1,249 mi)
First Stage (SSME with external tank) Main engines: Three Rocketdyne Block II SSMEs, each with a sea level thrust of 393,800 lbf (1.752 MN) at 104% power
Thrust (at liftoff, sea level, 104% power, all 3 engines): 1,181,400 lbf (5.255 MN)
Specific impulse: 455 s
Burn time: 480 s
Fuel: Liquid Oxygen/Liquid Hydrogen
Second Stage Engines: 2 Orbital Maneuvering Engines
Thrust: 53.4 kN (12,000 lbf) combined total vacuum thrust
Specific impulse: 316 s
Burn time: 1250 s
The rocket boys seem to think that just because the decreasing mass associated with the burning fuel allows the rocket to accelerate (gain velocity as opposed to maintaining a constant velocity) that–somehow – this magically allows the rocket to accelerate to a velocity greater than that of its exhaust– which is typical NASA nonsense. It can accelerate, but not beyond the velocity of its own exhaust. Acceleration and maximum velocity are apples and oranges.
led an American lodge of Crowley’s magical order, Ordo Templi Orientis (O.T.O.)
principal founders of the Jet Propulsion Laboratory
The Shuttle has a whole host of problems associated with its airframe shape (tail section, leading edges/wing width/construction – and other details) and function of the shock wave (heat from the compression of the air resulting from the shockwave accompanied by stagnant subsonic flow at supersonic speeds), and of materials/epoxy able to cope with the kinetic heating and drag.
The Shuttle’s (TPS) is the barrier that protected the Shuttle Orbiter during the searing 1,650 °C (3,000 °F) heat of atmospheric reentry (especially on the aluminium frame because the orbiter’s aluminum structure could not withstand temperatures over 175 °C (347 °F) without structural failure.)
1,668 °C – Titanium, Melting point (90 percent of the SR-71 is titanium)
1000 degrees Fahrenheit equals degrees Celsius 537.78
The strength of epoxy adhesives is degraded at temperatures above 350 °F (177 °C).
The SR-71’s heat generated during flight can reach over 1000 degrees F., with an average of over 600 degrees, that causes the fuselage to expand in flight from 4 to 6 inches in length. The component parts of the Blackbird fit very loosely to allow for expansion at high temperatures. At rest on the ground fuel leaks out constantly, since the large tanks only seal at operating temperatures.
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