Nou, dat was best een heet hangijzer voor ze!!quote:Op dinsdag 7 maart 2017 21:56 schreef t4600c het volgende:
[..]
Dat is een standpunt maken for the sake of een standpunt maken. Want who cares?
Dat vonkt vast mooi, oneindig hoge stroom.quote:Op dinsdag 7 maart 2017 22:10 schreef t4600c het volgende:
Er is een probleem met nul-punt energie....
Als ik het heb begrepen, heeft het een nog lagere potentiaal dan de Aarde, grond, onze planeet. Waardoor je dus gewoon gratis Aarde kan gebruiken als spanningsdraad. Want inplaats van Fase (opgewekt door energiecentrale) -> Nul... kan je: Nul -> nul-punt-energie draad.
Immers: Nul van energie centrale = Nul stoppenkast = Nul WCD = Aarde.
Het Nul draad van de energie centrale is eigenlijk een veredelde aardelektrode.
Maar goed: Als je dus een energie potentiaal opwekt LAGER dan aarde... wil de gehele aarde zich ontlanden naar het nul-punt-energie contact. Er bestaat geen isolatie sterk genoeg om dat te vorkomen, je krijgt te maken met praktisch oneindig hoge stroom.
Dat ga ik iedergeval niet aansluiten
Wat? Die heb ik nog niet eerder gehoordquote:Op dinsdag 7 maart 2017 21:52 schreef Wantie het volgende:
[..]
Geweldig niet?
Ander standpunt was dat we officieel nog steeds onder nazi-regime vallen omdat een of ander document niet zou zijn ondertekend in 1945 en dus alle wetgeving van na die datum ongeldig is
Voor dat argument heb je helemaal geen raket nodig toch?quote:Op woensdag 8 maart 2017 16:58 schreef t4600c het volgende:
Rocket at 73 miles shows moon, which proofs the earth is not a globe. Moon would be behind Earth at time of recording.
Platte aarders zijn christen, dus wat in de koran staat telt niet.quote:Op woensdag 8 maart 2017 17:23 schreef t4600c het volgende:
"And it is He who created the night and the day and the sun and the moon; all [heavenly bodies] in an orbit are swimming." https://quran.com/21/33
So:
The day has an orbit free from others and swimming.
The night has an orbit free from others and swimming.
The sun has an orbit free from others and swimming.
The moon has an orbit free from others and swimming.
So;
We pre know the light as an event of movement of sun. But in fact, "lightness and darkness" are created objects like sun and moon.
With the difference of @t4600c, All rights reserved. 8)
Op 73 mijl hoogte was de maan op 14 juli 2004 gewoon zichtbaar tusen 04:00 en 15:00 uur.quote:Op woensdag 8 maart 2017 16:58 schreef t4600c het volgende:
Rocket at 73 miles shows moon, which proofs the earth is not a globe. Moon would be behind Earth at time of recording.
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 193 194 195 196 197 198 | ******************************************************************************* Revised: Jul 26, 2016 Moon / (Earth) 301 PHYSICAL PROPERTIES: Radius (IAU), km = 1737.4 Mass, 10^20 kg = 734.9 Radius (gravity), km = 1738.0 Geometric albedo = 0.12 Density, gm cm^-3 = 3.3437 GM, km^3/s^2 = 4902.80007 V(1,0) = +0.21 Surface gravity = 1.62 m s^-2 Earth/Moon mass ratio = 81.3005691 Farside crust. thick. = ~80 - 90 km Nearside crust. thick.= 58+-8 km Heat flow, Apollo 17 = 2.2+-.5 mW/m^2 Heat flow, Apollo 15 = 3.1+-.6 mW/m^2 k2 = 0.024059 Mean crustal density = 2.97+-.07g/cm^3 Magnetometer moment = 435+-15 Induced magnetic mom. = 4.23x10^22Gcm^3 DYNAMICAL CHARACTERISTICS: Mean angular diameter = 31'05.2" Orbit period = 27.321582 d Obliquity to orbit = 6.67 deg Eccentricity = 0.05490 Semi-major axis, a = 384400 km Inclination = 5.145 deg Mean motion, rad/s = 2.6616995x10^-6 Nodal period = 6798.38 d Apsidal period = 3231.50 d Mom. of inertia C/MR^2= 0.393142 beta (C-A/B), x10^-4 = 6.310213 gamma (B-A/C), x10^-4 = 2.277317 ******************************************************************************* ******************************************************************************* Ephemeris / WWW_USER Wed Mar 8 10:00:27 2017 Pasadena, USA / Horizons ******************************************************************************* Target body name: Moon (301) {source: DE431mx} Center body name: Earth (399) {source: DE431mx} Center-site name: (user defined site below) ******************************************************************************* Start time : A.D. 2014-Jul-14 00:00:00.0000 UT Stop time : A.D. 2014-Jul-15 00:00:00.0000 UT Step-size : 60 minutes ******************************************************************************* Target pole/equ : IAU_MOON {East-longitude +} Target radii : 1737.4 x 1737.4 x 1737.4 km {Equator, meridian, pole} Center geodetic : 245.000000,36.0000000,117.00000 {E-lon(deg),Lat(deg),Alt(km)} Center cylindric: 245.000000,5260.65377,3796.9626 {E-lon(deg),Dxy(km),Dz(km)} Center pole/equ : High-precision EOP model {East-longitude +} Center radii : 6378.1 x 6378.1 x 6356.8 km {Equator, meridian, pole} Target primary : Earth Vis. interferer : MOON (R_eq= 1737.400) km {source: DE431mx} Rel. light bend : Sun, EARTH {source: DE431mx} Rel. lght bnd GM: 1.3271E+11, 3.9860E+05 km^3/s^2 Atmos refraction: NO (AIRLESS) RA format : HMS Time format : CAL EOP file : eop.170307.p170529 EOP coverage : DATA-BASED 1962-JAN-20 TO 2017-MAR-07. PREDICTS-> 2017-MAY-28 Units conversion: 1 au= 149597870.700 km, c= 299792.458 km/s, 1 day= 86400.0 s Table cut-offs 1: Elevation (-90.0deg=NO ),Airmass (>38.000=NO), Daylight (NO ) Table cut-offs 2: Solar Elongation ( 0.0,180.0=NO ),Local Hour Angle( 0.0=NO ) ******************************************************************************************************************************** Date__(UT)__HR:MN R.A._(ICRF/J2000.0)_DEC Azi_(a-appr)_Elev APmag S-brt delta deldot S-O-T /r S-T-O ******************************************************************************************************************************** $$SOE 2014-Jul-14 00:00 * 20 58 48.77 -12 48 49.2 69.1255 -45.8307 -12.22 3.95 0.00242826650905 -0.2279855 157.4793 /L 22.4687 2014-Jul-14 01:00 * 21 01 52.23 -12 41 30.1 80.0227 -34.6269 -12.21 3.97 0.00242204990621 -0.2859413 156.7953 /L 23.1512 2014-Jul-14 02:00 * 21 04 44.88 -12 34 26.1 88.9712 -23.0362 -12.20 3.98 0.00241465148088 -0.3256642 156.1514 /L 23.7939 2014-Jul-14 03:00 C 21 07 25.21 -12 27 28.1 97.1544 -11.3690 -12.19 4.00 0.00240654501766 -0.3444336 155.5524 /L 24.3918 2014-Jul-14 04:00 Nm 21 09 52.42 -12 20 25.7 105.3435 0.1394 -12.18 4.01 0.00239825520225 -0.3407694 155.0004 /L 24.9428 2014-Jul-14 05:00 m 21 12 06.51 -12 13 09.0 114.1859 11.2368 -12.17 4.02 0.00239032586703 -0.3145785 154.4944 /L 25.4478 2014-Jul-14 06:00 m 21 14 08.32 -12 05 28.3 124.3594 21.5827 -12.17 4.03 0.00238328562173 -0.2672228 154.0306 /L 25.9108 2014-Jul-14 07:00 m 21 15 59.49 -11 57 15.2 136.6286 30.6685 -12.16 4.04 0.00237761300124 -0.2014883 153.6020 /L 26.3387 2014-Jul-14 08:00 m 21 17 42.40 -11 48 23.5 151.6961 37.7410 -12.16 4.05 0.00237370365579 -0.1214447 153.1992 /L 26.7408 2014-Jul-14 09:00 m 21 19 19.98 -11 38 49.1 169.6107 41.8400 -12.15 4.06 0.00237184228309 -0.0321931 152.8108 /L 27.1284 2014-Jul-14 10:00 m 21 20 55.55 -11 28 31.1 188.9560 42.1629 -12.14 4.06 0.00237218185377 0.0604845 152.4244 /L 27.5140 2014-Jul-14 11:00 Am 21 22 32.55 -11 17 31.1 207.2679 38.6392 -12.12 4.07 0.00237473216032 0.1505436 152.0275 /L 27.9100 2014-Jul-14 12:00 Nm 21 24 14.30 -11 05 53.6 222.8822 31.9932 -12.11 4.08 0.00237935886261 0.2321234 151.6083 /L 28.3282 2014-Jul-14 13:00 *m 21 26 03.73 -10 53 45.2 235.6644 23.1990 -12.09 4.09 0.00238579313873 0.2999748 151.1567 /L 28.7788 2014-Jul-14 14:00 *m 21 28 03.23 -10 41 14.3 246.2759 13.0565 -12.07 4.10 0.00239365096663 0.3498262 150.6648 /L 29.2694 2014-Jul-14 15:00 *m 21 30 14.42 -10 28 29.9 255.5055 2.1165 -12.05 4.11 0.00240246015467 0.3786578 150.1277 /L 29.8053 2014-Jul-14 16:00 * 21 32 38.16 -10 15 41.4 264.0686 -9.2469 -12.03 4.13 0.00241169264898 0.3848643 149.5432 /L 30.3883 2014-Jul-14 17:00 * 21 35 14.46 -10 02 57.4 272.6479 -20.7514 -12.00 4.14 0.00242079942640 0.3683077 148.9124 /L 31.0175 2014-Jul-14 18:00 * 21 38 02.52 -09 50 25.7 282.0362 -32.1269 -11.98 4.15 0.00242924539872 0.3302685 148.2390 /L 31.6893 2014-Jul-14 19:00 * 21 41 00.85 -09 38 12.5 293.3851 -43.0151 -11.95 4.17 0.00243654210719 0.2733139 147.5292 /L 32.3974 2014-Jul-14 20:00 * 21 44 07.36 -09 26 22.4 308.6021 -52.7830 -11.93 4.18 0.00244227645805 0.2011040 146.7913 /L 33.1337 2014-Jul-14 21:00 * 21 47 19.48 -09 14 58.2 330.4762 -60.1556 -11.90 4.20 0.00244613423211 0.1181541 146.0349 /L 33.8885 2014-Jul-14 22:00 * 21 50 34.35 -09 04 00.7 359.6646 -62.9946 -11.88 4.22 0.00244791752240 0.0295703 145.2708 /L 34.6509 2014-Jul-14 23:00 * 21 53 48.93 -08 53 29.1 28.6797 -59.9469 -11.86 4.23 0.00244755558180 -0.0592325 144.5102 /L 35.4100 2014-Jul-15 00:00 * 21 57 00.22 -08 43 21.0 50.2641 -52.4178 -11.84 4.25 0.00244510879887 -0.1428184 143.7641 /L 36.1548 $$EOE ******************************************************************************************************************************** Column meaning: TIME Prior to 1962, times are UT1. Dates thereafter are UTC. Any 'b' symbol in the 1st-column denotes a B.C. date. First-column blank (" ") denotes an A.D. date. Calendar dates prior to 1582-Oct-15 are in the Julian calendar system. Later calendar dates are in the Gregorian system. Time tags refer to the same instant throughout the solar system, regardless of where the observer is located. For example, if an observation from the surface of another body has an output time-tag of 12:31:00 UTC, an Earth-based time-scale, it refers to the instant on that body simultaneous to 12:31:00 UTC on Earth. The Barycentric Dynamical Time scale (TDB) is used internally as defined by the planetary equations of motion. Conversion between TDB and the selected non-uniform UT output time-scale has not been determined for UTC times after the next July or January 1st. The last known leap-second is used as a constant over future intervals. NOTE: "n.a." in output means quantity "not available" at the print-time. SOLAR PRESENCE (OBSERVING SITE) Time tag is followed by a blank, then a solar-presence symbol: '*' Daylight (refracted solar upper-limb on or above apparent horizon) 'C' Civil twilight/dawn 'N' Nautical twilight/dawn 'A' Astronomical twilight/dawn ' ' Night OR geocentric ephemeris LUNAR PRESENCE (OBSERVING SITE) The solar-presence symbol is immediately followed by a lunar-presence symbol: 'm' Refracted upper-limb of Moon on or above apparent horizon ' ' Refracted upper-limb of Moon below apparent horizon OR geocentric ephemeris R.A._(ICRF/J2000.0)_DEC = J2000.0 astrometric right ascension and declination of target center. Adjusted for light-time. Units: HMS (HH MM SS.ff) and DMS (DD MM SS.f) Azi_(a-appr)_Elev = Airless apparent azimuth and elevation of target center. Adjusted for light-time, the gravitational deflection of light, stellar aberration, precession and nutation. Azimuth measured North(0) -> East(90) -> South(180) -> West(270) -> North (360). Elevation is with respect to plane perpendicular to local zenith direction. TOPOCENTRIC ONLY. Units: DEGREES APmag S-brt = Moon's approximate apparent visual magnitude & surface brightness. When phase angle < 7 deg (within ~ 1 day of full Moon), computed magnitude tends to be about 0.12 too small. Units: MAGNITUDE & VISUAL MAGNITUDES PER SQUARE ARCSECOND delta deldot = Range ("delta") and range-rate ("delta-dot") of target center with respect to the observer at the instant light seen by the observer at print-time would have left the target center (print-time minus down-leg light-time); the distance traveled by a light ray emanating from the center of the target and recorded by the observer at print-time. "deldot" is a projection of the velocity vector along this ray, the light-time-corrected line-of-sight from the coordinate center, and indicates relative motion. A positive "deldot" means the target center is moving away from the observer (coordinate center). A negative "deldot" means the target center is moving toward the observer. Units: AU and KM/S S-O-T /r = Sun-Observer-Target angle; target's apparent SOLAR ELONGATION seen from the observer location at print-time. Angular units: DEGREES The '/r' column indicates the target's apparent position relative to the Sun in the observer's sky, as described below: For an observing location on the surface of a rotating body (considering its rotational sense): /T indicates target TRAILS Sun (evening sky; rises and sets AFTER Sun) /L indicates target LEADS Sun (morning sky; rises and sets BEFORE Sun) For an observing point NOT on a rotating body (such as a spacecraft), the "leading" and "trailing" condition is defined by the observer's heliocentric orbital motion: if continuing in the observer's current direction of heliocentric motion would encounter the target's apparent longitude first, followed by the Sun's, the target LEADS the Sun as seen by the observer. If the Sun's apparent longitude would be encountered first, followed by the target's, the target TRAILS the Sun. NOTE: The S-O-T solar elongation angle is numerically the minimum separation angle of the Sun and target in the sky in any direction. It does NOT indicate the amount of separation in the leading or trailing directions, which are defined in the equator of a spherical coordinate system. S-T-O = "S-T-O" is the Sun->Target->Observer angle; the interior vertex angle at target center formed by a vector to the apparent center of the Sun at reflection time on the target and the apparent vector to the observer at print-time. Slightly different from true PHASE ANGLE (requestable separately) at the few arcsecond level in that it includes stellar aberration on the down-leg from target to observer. Units: DEGREES Computations by ... Solar System Dynamics Group, Horizons On-Line Ephemeris System 4800 Oak Grove Drive, Jet Propulsion Laboratory Pasadena, CA 91109 USA Information: http://ssd.jpl.nasa.gov/ Connect : telnet://ssd.jpl.nasa.gov:6775 (via browser) telnet ssd.jpl.nasa.gov 6775 (via command-line) Author : Jon.Giorgini@jpl.nasa.gov ******************************************************************************************************************************** |
SPOILEROm spoilers te kunnen lezen moet je zijn ingelogd. Je moet je daarvoor eerst gratis Registreren. Ook kun je spoilers niet lezen als je een ban hebt.
daarom zei ik in het vorige topic al, als je een raket nu omhoog knal word het weer licht.quote:Op woensdag 8 maart 2017 16:58 schreef t4600c het volgende:
Rocket at 73 miles shows moon, which proofs the earth is not a globe. Moon would be behind Earth at time of recording.
Dat is een broodje aap manquote:Op dinsdag 7 maart 2017 15:53 schreef motorbloempje het volgende:
Is het trouwens al voorbij gekomen dat een waterkolk de andere kant op draait aan de andere kant van de aarde?
Klopt, snipers daarentegen moeten er wel rekening mee houden dat hun kogel afbuigt op grote afstand.quote:Op donderdag 9 maart 2017 00:11 schreef starla het volgende:
[..]
Dat is een broodje aap man
Het corioliseffect is verwaarloosbaar op zo'n kleine schaal.
Religie.quote:Op donderdag 9 maart 2017 08:25 schreef motorbloempje het volgende:
Wat ik me vooral afvraag is wat het nut zou zijn van deze conspiracy.… dus, waarom zou het zo erg zijn dat de aarde plat is en dat we daarom moeten geloven dat het een sphere is.
het corioliseffect is wel zichtbaar in weerpatronen, zoals orkanen.quote:Op donderdag 9 maart 2017 00:51 schreef de_tevreden_atheist het volgende:
[..]
Klopt, snipers daarentegen moeten er wel rekening mee houden dat hun kogel afbuigt op grote afstand.
Goede vraag.quote:Op donderdag 9 maart 2017 12:27 schreef motorbloempje het volgende:
Oh, en de langere nachten/dagen in het hoge Noorden, enzo, hoe wordt dat eigenlijk uitgelegd?
Deze vraag stelde ik een tijd geleden ook al eens.quote:Op donderdag 9 maart 2017 12:27 schreef motorbloempje het volgende:
Oh, en de langere nachten/dagen in het hoge Noorden, enzo, hoe wordt dat eigenlijk uitgelegd?
Dat ontkent hij toch ook niet?quote:Op donderdag 9 maart 2017 11:03 schreef t4600c het volgende:
[..]
het corioliseffect is wel zichtbaar in weerpatronen, zoals orkanen.
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