It looks like you're using an Ad Blocker.
Please white-list or disable AboveTopSecret.com in your ad-blocking tool.
Thank you.
Some features of ATS will be disabled while you continue to use an ad-blocker.
Originally posted by JimOberg
Originally posted by EvolvedMinistry
But, as I said before...because you lack any mathematical skills where you can demonstrate and illuminate these "supposed" fundamental flaws, your opinion of whether it is valid or not is NULL AND VOID. As a matter of fact, I have yet to see you post any evidence on your behalf whatsoever...
Here's where you admitted no mathematical skills.....
As a guy with advanced mathematical skills as validated by graduate degrees, I can't judge your opponent's 'skills', but his 'mathematical intuition' [a key factor in the best theoretical mathematics] seems excellent to me. "Maths" is what we say too -- if you think it's 'childish' or a misnomer, it's you who's being exposed, not him.
When you too can raise 'e' to the '2 pi i' power and get a real number,
maybe people will learn some respect for your own claimed maths talents.
Originally posted by JimOberg
As a guy with advanced mathematical skills as validated by graduate degrees, I can't judge your opponent's 'skills', but his 'mathematical intuition' [a key factor in the best theoretical mathematics] seems excellent to me. "Maths" is what we say too -- if you think it's 'childish' or a misnomer, it's you who's being exposed, not him.
When you too can raise 'e' to the '2 pi i' power and get a real number,
maybe people will learn some respect for your own claimed maths talents.
"... after the Second World War, scientists started to explore radio wave heating techniques for modifying ionospheric conditions. The first megawatt-range heating facilities were built in the 1970s (Platteville, Colorado, USA and SURA, Novgorod, USSR). Especially the usage of a periodically heated ionosphere as a large-scale an tenna for electromagnetic wave generation at low frequencies was studied extensively. In the USA as well as the former USSR, this research was motivated by the military requirement to communicate with deeply submerged submarines, although in practise, the capability of heating facilities for this purpose turned out to be insufficient [Barr, 1998]. However, scientific usage of active heating techniques expanded to various fields, some of them introduced in Section 1.2. New facilities were built for these purposes in the 1980s (Arecibo, Puerto Rico, USA; Troms¿, Norway; HIPAS, Alaska, USA) and most recently HAARP in Alaska, USA (1995) and SPEAR in Svalbard (2003) ...."
Are you aware that, in your previous thread you calculated the altitude of the whole spiral event to never surpass 453 kms, with the center, were the missile would be, at max 296.5 kms. The whole event takes place below the third stage level of a Bulava missile, according to your own post.
Originally posted by Point of No Return
reply to post by tauristercus
Tauresticus, I must say I'm a bit dissapointed that you didn't reply to my post were I made this point:
Are you aware that, in your previous thread you calculated the altitude of the whole spiral event to never surpass 453 kms, with the center, were the missile would be, at max 296.5 kms. The whole event takes place below the third stage level of a Bulava missile, according to your own post.
To me, this seems like a pretty important piece of evidence, why is this ignored?
I expected this to be of interest to you, maybe i was wrong.
Or did you just miss that post?
Originally posted by Point of No Return
reply to post by EvolvedMinistry
Thanks.
It's amazing that noone else even wants to acknowledge this finding.
I guess one can try to ignore something and hope it will go away.
It just starts to look bad when people keep ignoring valid points.
The 28-foot first-stage solid-fuel rocket motor weighed approximately 108,000 pounds and is capable of boosting the missile to about 75,000 feet. The 18-foot long second-stage motor propelled the missile to an altitude of about 190,000 feet and weighed 60,000 pounds. The rocket motor in the eight-foot third stage weighed 17,000 pounds and supplied the thrust to boost the missile to about 700,000 feet. The 2,300 pound post-boost fourth stage vehicle was designed to maneuver the missile into position for the multiple reentry vehicles to deploy in their respective ballistic trajectories.
The ICBM gained speed. Within a minute, the rocket had accelerated to nearly 5,000 mph and reached an altitude of 100,000 feet.
Another flash of light marked the sky as the rocket’s second stage ignited and the first was jettisoned. The spent first stage fell earthward, its red-hot tail tumbling end over end.
Two minutes into the flight, GT-198 was traveling more than 10,000 mph. It had reached an altitude of 350,000 feet and was 120 miles downrange, but was still clearly visible in the night sky.
As the third stage ignited and the second fell toward Earth, the rocket roared toward its top speed of nearly 15,000 mph. At 750,000 feet, a platform holding the dummy warhead was in low orbit.
Originally posted by Point of No Return
reply to post by tauristercus
Tauresticus, I must say I'm a bit dissapointed that you didn't reply to my post were I made this point:
Are you aware that, in your previous thread you calculated the altitude of the whole spiral event to never surpass 453 kms, with the center, were the missile would be, at max 296.5 kms. The whole event takes place below the third stage level of a Bulava missile, according to your own post.
To me, this seems like a pretty important piece of evidence, why is this ignored?
I expected this to be of interest to you, maybe i was wrong.
Or did you just miss that post?
So that original thread and my deductions linking Norway and EISCAT to the event was just plain wrong ... wrong ... wrong ... and I acknowledged clearly and openly as much in the opening post of my new thread "Norway Spiral : Case reopened - an analysis of an event". With the wealth of much more photographic evidence having been made available since that original thread, I basically decided that the best policy from my point of view would be to literally throw away and discard all the previous potentially inaccurate data that I had used and go back to the drawing board and re-analyze the event completely anew using these newly available data sources.
When I created that 1st thread, I had to search around to try and locate some info on just how high a Bulava could go and the only instance I found stated that a Bulava has an apogee (max altitude) of 1000 kms. Now because that was all we were told, and because there were 3 stages involved, I decided to use an approximation that the combined first 2 stages pushed the Bulava up to around 2/3rds of the apogee (500 to 600 kms) and the final stage pushed it the remaining distance ... hence my initial estimate that the 3rd stage would fire up somewhere above the 500 km mark.
www.astronautix.com...
Submarine-launched ballistic missile area known to have been used for 27 launches from 1955 to 2007, reaching up to 1000 kilometers altitude.
2007 June 28 - Launch Vehicle: Bulava. Bulava SLBM test Agency: VMF. Apogee: 1,000 km (600 mi). The warhead impacted on target in the Kamchatka Peninsula. This was the first successful launch after two consecutive failures.