you want your station to broadcast. A full-power station will need tens of thousands of watts‚ while a low-power station may only need a thousand watts. 4. Buy the necessary equipment‚ including transmitter gear and an antenna. You may need to rent space on a tower for your antenna. 5. Design your studio. You’ll need sound proofing‚ headphones‚ speakers‚ microphones and more 6. [source: Community-Media]. 7. Recruit broadcasters. Make sure you have enough people to fill up all the time slots. 8
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(C3) to capture the RF signals from the mobile phone. The lead length of the capacitor is fixed as 18 mm with a spacing of 8 mm between the leads to get the desired frequency. The disk capacitor along with the leads acts as a small gigahertz loop antenna to
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used‚ importantly‚ the battery needs to be charged first before taking it anywhere. This is done by use of microwaves. The microwave signal is transmitted from the transmitter along with the message signal using special kind of antennas called slotted wave guide antenna at a frequency is 2.45 GHz. There are minimal additions‚ which have to be made in the mobile handsets‚ which are the addition of a sensor‚ a Rectenna‚ and a filter. With the above setup‚ the need for separate chargers for mobile
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Kropotkin’s ideas revolve largely around cooperation characterised by the organizations aforementioned. This essay will explore Hobbes and Kropotkin’s ideas in more detail in order to derive if they are relevant today with close reference to Scott Tuners article ‘Global civil society‚ anarchy and governance’. To derive to what extent Hobbes and Kropotkin’s theories are applicable to modern day societies their key ideas must be understood; Hobbes’ anarchist argument is structured around the belief
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solar system has a different density of the atmosphere outside our atmosphere‚ the PSL would have confirmed Voyager 1’s exact whereabouts. The Voyager does however have two functioning antennas that detected abnormal vibrations‚ leading scientists to believe its debut into interstellar space. Those same two antenna have also recently detected oscillations (variations in magnitude or position) that suggest the surrounding plasma was cold and dense. Scientist Ed Stone addresses this information to be
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Zigbee and Xbee ZigBee is a standard defined by the IEEE ( Institure of Electrical and Electronics Engineers) back in 1998. When a group of big guy say WiFi and Bluetooth might not be suitable enough for some applications‚ they started to define new protocol‚ new standard. ZigBee aim to have lower data rate compared to Bluetooth‚ at 250Kbps (Bluetooth is 1Mbps back then‚ now is higher with EDR-Enhanced Data Rate). More importantly‚ ZigBee aims for lower power applications which should offer years
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adapt to changing functional uses without losing one bit of its dignity or one bit of its original intention. And I think that’s the great thing about the building at the end of the day” (Frank Lloyd Wright: From Within Outward Audioguide [New York: Antenna Audio‚ Inc. and the Solomon R. Guggenheim Foundation‚ 2009]). Up to the very end of his life‚ Wright carried on a battle to be sure that the Guggenheim embodied his belief in the unity of form and function. On July 15‚ 1958‚ less than a year before
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Wireless communication protocols have evolved rapidly since the introduction of 802.11 Legacy over a decade ago. Over the last 10 years we have seen efficiency and performance increases on all fronts‚ which have lead to greater range and faster transfer speeds. With Legacy 802.11 protocols‚ speeds maxed out at around 2 Mbits/sec and indoor range was only about 20 meters. In 1999‚ the 802.11 protocol got a couple of amendments in the form of 802.11a and 802.11b. Both offered higher speeds and slightly
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Feasibility Study of Automatic Attendance System Using RFID A report submitted to Amity University as a part fulfillment of Full time MBA Telecom |Submitted To: |Submitted By: | | | | |Prof. Marshal Sahni
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Mars Orbiter Mission Mars Orbiter Mission Artist’s rendering of the MOM orbiting Mars Mission type Mars orbiter Operator ISRO COSPAR ID 2013-060A SATCAT № 39370 Website www.isro.org/mars/home.aspx Mission duration 300 days Spacecraft properties Bus I-1K[1] Manufacturer ISAC Launch mass 1‚337 kg (2‚948 lb)[2] Dry mass 500 kg (1‚100 lb)[3] Payload mass 15 kg (33 lb)[4] Dimensions 1.5 metres (4 ft 11 in) cube Power 840 watts[1] Start of mission Launch date 5 November 2013‚ 09:08 UTC[5]
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