Unreferenced date December 2009 Image Loki.jpg thumb The sounding rocket Loki with dart A dart is a free flying top of a sounding rocket , and contains the Payload air and space craft payload . Its form is very aerodynamics aerodynamically designed. After the launch stage burned out the dart is detached and continues to rise only with its own inertia . Some sounding rockets are available both with or without dart. The version without dart is able to transport more payload, but reaches lesser height. Applications Mohr Rocket MMR06 Loki rocket Loki Dart Meteor rocket Meteor DEFAULTSORT Dart Rocketry Category Meteorological instrumentation and equipment Rocket stub de Dart Raketentechnik ... more details
unreferenced date October 2007 In information technology , trailer refers to supplemental data placed at the end of a block of data being stored or transmitted, which may contain information for the handling of the data block, or just mark its end. In data transmission, the data following the end of the Header information technology header and preceding the start of the trailer is called the Payload computing payload or body. It is vital that trailer composition follow a clear and unambiguous specification or File format format , to allow for parsing . If a trailer is not removed properly, or part of the payload is removed thinking it is a trailer, it can cause confusion. Examples In data transfer, the OSI data link layer adds a trailer at the end of the data encapsulating. Category Computer data compu storage stub ... more details
investigator s teams payload development teams are to be deployed at ISSDC to support ... centers, Payload designers, Payload operations centers, Principal investigators, Mission software ... more details
Channel associated signaling CAS , also known as per trunk signaling PTS , is a form of digital communication Signaling telecommunications signaling . As with most telecommunication signaling methods, it uses routing information to direct the payload of voice or data to its destination. With CAS signaling, this routing information is encoded and transmitted in the same channel as the payload itself. This information can be transmitted in the same band in band signaling or a separate band out of band signaling to the payload. CAS potentially results in lower available bandwidth for the payload. For example, in the PSTN the use of out of band signaling within a fixed bandwidth reduces a 64 kbit s DS0 to 56 kbit s. Because of this, and the inherent security benefits of separating the control lines from the payload, telephone systems introduced since the 1960s rely more on common channel signaling CCS . ref cite book title Signaling in telecommunication networks edition 2nd author John G. Van Bosse and Fabrizio U. Devetak publisher John Wiley and Sons year 2007 isbn 9780471662884 page 111 url http books.google.com books?id avTW90pQC1MC&pg PA111 ref The most common implementation of CAS is robbed bit signaling . References reflist telecom stub Category Telecommunications standards de Channel Associated Signalling ... more details
Earth to Orbit ETO describes the process or means of placing a Payload air and space craft payload into an orbit around the Earth . Traditionally this has used rockets, however ETO can also include much more exotic forms of transportation such as railgun s and hypersonic cannon s and Space elevator s. Methods Earth to orbit transportation can be roughly broken up into four groups, these are Rocket transportation Ballistic methods Orbital transportation Relay transportation Rocket Based Transportation image Gemini VI Launch GPN 2000 000612.jpg thumb right 200px Titan II Rocket Launch A series of suborbital rocket s are used in order to accelerate a payload to orbital velocities. This is the only method of placing a payload into an earth orbit which has been successfully used. It involves constructing a series of rockets which are usually stacked on one another, imparting their change in momentum to the payload before dropping away. Although a series of suborbital rockets are usually used. Other schemes involving SSTO or Single Stage To Orbit vehicles have been proposed. However they all suffer from a low Mass fraction , reducing their effectiveness for transporting payloads into orbit. Ballistic methods A stationary platform at least partly in Earth s atmosphere that delivers the required momentum by using the Earth to react against. Examples of this may be a railgun , coil gun s, or a hypervelocity gun . Because the payload is accelerated to velocities greater than required for orbital velocity by the time the payload has left the device, either very high accelerations are required ... the payload to orbital velocities. The most accepted candidates used various configurations of a Tether . The most promising is the Skyhook elevator which uses momentum exchange to boost the payload ... exchange tether to the payload it loses orbital energy, decreasing in altitude. The loss in altitude ... per Pound of Payload br Category Spacecraft propulsion Space stub ... more details
multiple issues cleanup September 2011 unreferenced August 2011 Overview An .ipa file is an iPhone application archive file which stores an iPhone app . It is usually encrypted with Apple Inc. Apple s FairPlay Digital rights management DRM technology. Each .ipa file is compressed with a binary for the ARM architecture and can only be installed on an iPhone, iPod Touch , or iPad . Files with the .ipa extension can be uncompressed by changing the extension to ZIP file format .zip and unzipping. br .ipa files cannot be installed on the iPhone Simulator because they do not contain a binary for the x86 architecture. To run applications on the simulator, original project files which can be opened using the Xcode SDK are required. Vulnerabilities An unsigned .ipa can be created by copying the file with the extension APP file format .app from the Products folder of the application in Xcode to a folder called Payload computing Payload and compressing the latter using the command code zip 9 y r myAppName.ipa Payload code It is then possible to install unsigned .ipa files on iOS jailbreaking jailbroken devices using third party software like Appsync. Structure of the IPA An IPA has a built in structure for iTunes and App Store iOS AppStore to recognize, The example below shows the structure of an IPA code Payload br Payload Application.app br iTunesArtwork br iTunesMetadata.plist code As shown above, the Payload computing Payload folder is what contains all the app data. The iTunes Artwork file is a 512x512 pixel Portable Network Graphics PNG image, containing the app s icon for showing in iTunes and the App Store app on the iPad . The iTunesMetadata.plist contains various bits of information, ranging from the developer s name and ID e.g., Google , the bundle identifier, copyright information, genre, the name of the app, release date, purchase date, etc. DEFAULTSORT Ipa Category Filename extensions technology stub es .ipa it IPA formato di file ru .ipa ... more details
payload 5500 kg payload TLS PL name flagicon USSR 1955 Kosmos 1070 user function orbit Low Earth orbit ... pad LSP flagicon USSR 1955 remarks Military payload 6000 kg payload TLS PL name flagicon USSR 1955 ... flagicon USSR 1955 Plesetsk Cosmodrome unknown pad LSP flagicon USSR 1955 remarks Military payload 810 kg payload TLS PL name flagicon USSR 1955 Kosmos 1072 user function orbit Low Earth orbit Low ... flagicon USSR 1955 remarks Civilian payload 1750 kg payload TLS PL name flagicon USSR 1955 Molniya ... USSR 1955 remarks Civilian payload 1100 kg payload TLS PL name flagicon USSR 1955 Meteor prigoda 2 Meteor ... payload 659 kg payload TLS PL name flagicon USA 1955 SCATHA user function orbit Highly elliptical ... Cosmodrome unknown pad LSP flagicon USSR 1955 remarks Military payload 6000 kg payload TLS PL ... Military payload 7000 kg payload TLS PL name flagicon USSR 1955 Kosmos 1074 user function orbit ... Space Center Tanegashima , Osaki launch complex LSP flagicon Japan 1955 remarks Civilian payload 260 kg payload TLS PL name flagicon Japan 1955 Ayame 1 ECS A user function orbit Highly elliptical ... Military payload 1080 kg payload TLS PL name flagicon USSR 1955 Kosmos 1075 user function orbit ... Cosmodrome pad LC 32 2 LSP flagicon USSR 1955 remarks Military payload 1900 kg payload TLS PL ... remarks Military payload 2500 kg payload TLS PL name flagicon USSR 1955 Kosmos 1077 user function orbit ... Cosmodrome pad LC 41 LSP flagicon USSR 1955 remarks Military payloadpayload TLS PL name flagicon USSR ... remarks Civilian payload 147 kg payload TLS PL name flagicon USA 1955 SAGE Disambiguation needed ... Center Tanegashima , Mu launch complex LSP flagicon Japan 1955 remarks Civilian payload 100 kg payload ... , pad LC 200P pad 40 LSP flagicon USSR 1955 remarks Civilian payload 1970 kg payload TLS PL name flagicon ... USSR 1955 Plesetsk Cosmodrome unknown pad LSP flagicon USSR 1955 remarks Military payload 6000 kg payload ... pad SLC 3 SLC 3W LSP flagicon USA 1955 remarks Military payload 1331 kg payload TLS PL name flagicon ... more details
Throw weight is a measure of the effective weight of ballistic missile Payload air and space craft payload s. It is measured in kilograms or metric ton s. Throw weight equals the total weight of a missile s warhead s, reentry vehicle s, self contained dispensing mechanisms, penetration aids , and guidance system s generally all components except for the launch rocket booster and launch fuel. Throw weight was used as a criterion in classifying different types of missiles during Strategic Arms Limitation Talks between the Soviet Union and the United States . ref James John Tritten, http www.airpower.maxwell.af.mil airchronicles aureview 1982 nov dec tritten.html Throw Weight and Arms Control Bot generated title , Air University Review , Nov Dec 1982. ref See also Payload air and space craft Troop density References references Category Ballistic missiles Category Intercontinental ballistic missiles Category Military science nuclear weapon stub Mil hist stub ca Pes llan able fr Capacit d emport pl Throw weight ... more details
refimprove date November 2011 Win9x. Shoerec is a Win32 encrypted parasitic computer virus . It is a direct action virus. Effects The virus activates its payload after three to four months from the first infection. It exploits the Windows Desktop and mouse Device driver drivers , and makes icons run away from the cursor creating a hilarious, and an annoying payload. If files are infected in 1st, 2nd, or 3rd of any month, the virus may add another destructive payload into it. After seven months of such infection, the virus erases all files in the drive and may create a WIN.COM file this may contain garbage or a clear text, as such pre c 1999 Brain & Amjads pvt Ltd VIRUS SHOE RECORD v20.0 Dedicated to the dynamic memories of millions of virus who are no longer with us today Thanks pre See also List of computer viruses S Z External links http www.securelist.com en descriptions old20063 SecureList description about Shoerec Category Windows viruses Compu prog stub malware stub ... more details
MR 20 is a Russia n sounding rocket . The MR 20 is 9 meters long, has a diameter of 45 centimeters, and can bring a payload of 130 kilograms to a height of 250 kilometers. External links http www.astronautix.com lvs mr20.htm Category Sounding rockets of the Soviet Union rocket stub de MR 20 es MR 20 ja MR 20 ... more details
The mass fraction may refer to Propellant mass fraction , in aerospace engineering , the amount of mass left behind such as the stages of rocket s Payload fraction , also in aerospace engineering, characterizes the efficiency of the mass to be transported compared to the total mass Mass fraction chemistry , the ratio or percentage of one substance out of the total disambig de Massenanteil ... more details
Elrad may refer to Earth Limb Radiance Experiment, a secondary payload of the 26th Space Shuttle mission, STS 26 elrad magazine , a discontinued semi professional electronic magazine in Germany Tzilla Elrad , technical author Long Range Acoustic Device or LRAD pronounced el rad disambig ... more details
PDRS may refer to Payload Deployment and Retrieval System Probe Data Relay Subsystem disambig Short pages monitor This long comment was added to the page to prevent it from being listed on Special Shortpages. It and the accompanying monitoring template were generated via Template Long comment. Please do not remove the monitor template without removing the comment as well. ... more details
Unreferenced date December 2011 The E56 120 mm Mortar , is a Heavy Infantry mortar referred to as such by its 120 mm payload, produced by the Hellenic Arms Industry for the Hellenic Army . Category 120 mm artillery Category Infantry mortars Category Modern weapons of Greece Category Hellenic Army Greece mil stub ... more details
recovery of payload from KSC File STS 40 GBA.jpg thumb STS 40 Gas Bridge Assembly with G 616 GAS canister .... Small Self Contained Payload G 616 was managed and owned by Thomas M Hancock III a space scientist ... the primary payload. It was approved for flight by NASA in 1988. G 616 originally consisted of 3 ... creating significant debris. The other two experiments passed testing and payload safety data reviews ... worked with every school in the Redlands Unified School District in support if this effort. The payload was integrated KSC in early 1990 and was the 1st Shuttle Small Payload constructed and assembled ... Shuttle main propulsion system delayed launch for over 1 year. During this time the payload was stored on the GAS Bridge Assembly ready for flight Hangar AF, NASA KSC. On June 5th 1991 the payload ... 1 . The payload spent 9 days in orbit landing at Edwards Air Force Base. The payload was recovered .... Papers about the experiments where published in the 1988, 1993 and 1999 the Shuttle Small Payload ... of the payload canister during the mission. File Sts 40 post flight letter.jpg thumb Proof ... Report. G 616 payload listing. See page 2 6 Category NASA programs ... more details
information above the 60,000 foot limit imposed upon manufacturers, as well as the payload enclosure and antenna system to be used for future flights. A Pooh Bear mascot was also included in the payload ... 10 22 ref ref http bear.sbszoo.com bear1 2 images b2 b2 news.gif ref This payload contained the same ..., Red Deer, Calgary corridor in Alberta. A last minute addition to the payload was an inexpensive ... turned off for the flight. The hole in the payload container for the camera ended ... in the series to be filled with hydrogen instead of helium. The payload contained a Trimble Lassen iQ ... ref A custom payload enclosure was designed in an effort to attempt to produce an ultra light weight payload. A payload mass of 95.8 grams was achieved which puts it tied with the lightest payload in the http www.arhab.org ARHABrecords.htm Amateur Radio High Altitude Ballooning Records . This payload ... Kamiko from Japan. Tomoya provided the camera, while the BEAR team provided the payload container, tracking hardware, parachute and balloon. This payload was recovered near Mannville, Alberta. BEAR ... more details
Taurus Tomahawk , in rocket rocketry is a two stage elevator sounding rocket , consisting of a Taurus rocket Taurus starting stage and a TE 416 Tomahawk upper stage. Taurus Tomahawks were used between 1978 and 1987. The Taurus Tomahawk could carry 27 kilograms of Payload air and space craft payload to an altitude of 590 kilometers. The launch thrust of the Taurus Tomahawk amounted to 457 Kilonewton s, the launch weight 1.611 tons, the diameter of 0.58 meters and the overall length of 9.38 meters. External links http www.astronautix.com lvs tauahawk.htm Taurus Tomahawk Category Sounding rockets of the United States de Taurus Tomahawk rocket stub ... more details
Unreferenced date December 2009 Orphan date December 2009 The satellite revisit time is the time elapsed between observations of the same point on earth by a satellite . It depends on the satellite s orbit, target location, and swath of the sensor. Revisit is related to the same ground trace a projection on to the earth of the satellite s orbit. Revisit requires a very close repeat of the Ground Trace. In the case of polar hi inclination low earth orbiting reconnaissance satellites, the sensor payload must have the variable swath to look longitudinally east west, or sideways at a target, in addition to direct overflight observation, looking nadir . In the case of the Israel i EROS satellite EROS earth observation satellite, the ground trace repeat is 15 days, but the actual revisit time is 3 days, because of the swath ability of the camera payload. DEFAULTSORT Satellite Revisit Category Satellites ... more details
Infobox software name Twinkle logo File Twinkle logo.png 100px screenshot Image Twinkle 1.4.2 en.png 200px caption collapsible author developer Michel de Boer released 27 April 2005 frequently updated yes Release version update? Don t edit this page, just click on the version number programming language C graphical interface Qt framework Qt 3 operating system GNU Linux platform size language status genre Voice over IP VoIP license GNU General Public License website http www.twinklephone.com www.twinklephone.com Twinkle is a free software free and open source software application for Voice over Internet Protocol VoIP voice communications in IP networks, such as the Internet . ref http www.twinklephone.com Twinklephone Website ref It is designed for GNU Linux operating systems and uses the Qt framework Qt toolkit for its graphical user interface. For call signaling it employs the Session Initiation Protocol SIP . It also features direct IP to IP calls. Media streams are transmitted via the Real time Transport Protocol RTP which may be encrypted with the Secure Real time Transport Protocol SRTP and the ZRTP security protocols. Since version 1.3.2 September 2008 , Twinkle supports message exchange and a buddy list feature for presence notification, showing the online status of predefined communications partners provider support needed . Supported audio formats G.711 A law 64 kbit s payload, 8 kHz sampling rate G.711 law 64 kbit s payload, 8 kHz sampling rate G.726 16, 24, 32 or 40 kbit s payload, 8 kHz sampling rate GSM 06.10 GSM 13 kbit s payload, 8 kHz sampling rate iLBC 13.3 or 15.2 kbit s payload, 8 kHz sampling rate Speex narrow band 15.2 kbit s payload, 8 kHz sampling rate Speex wide band 28 kbit s payload, 16 kHz sampling rate Speex ultra wide band 36 kbit s payload, 32 kHz sampling rate See also Portal Free software Comparison of VoIP software List of SIP software Opportunistic encryption References Reflist External link ... more details
dablink This article is about a proposed enlarged Saturn V. For the Saturn V expendable launch vehicle ELV , see Saturn V unreferenced date August 2008 The Saturn V ELV was to be an enlarged Saturn V with the addition of four Titan UA1207 solid rocket boosters. Had it been built it would have been able to put a 200,000 kg payload into low earth orbit or a 67,000 kg payload into a translunar trajectory. Vehicle Layout class wikitable Zero Stage 1st Stage 2nd Stage 3rd Stage 4x Titan UA1207 MS IC 4 S B MS II 1A MS IVB 1A Saturns Category Saturn rocket family V ELV it Saturn V ELV ... more details
Primarysources date April 2007 Refimprove date April 2007 UCISAT is a student run CubeSat project at the University of California, Irvine . Satellites UCISAT 1 UCISAT 1 is the first pico satellite under development by the University of California, Irvine. The primary mission payload is a CMOS camera which will photograph the Earth from Low Earth Orbit and transmit images back to the K6UCI Ground Station. The secondary mission payload is a 6 DOF inertial measurement unit that will measure the spacecraft s rate of tumble from the time of deployment until it is stabilized by a passive magnetic attitude control system. External links http ucisat.eng.uci.edu index.html UCISAT Category Student satellites Category University of California, Irvine Category CubeSats ... more details
Use dmy dates date May 2011 STS 61 H was a United States Space Shuttle mission planned to launch in 1986 using Space Shuttle Columbia Columbia , however, it was cancelled after the Space Shuttle Challenger disaster Challenger disaster . The flight was scheduled to take place 24 June through 1 July. Crew Commander Michael L. Coats Pilot John Blaha Mission Specialist 1 Anna L. Fisher Mission Specialist 2 James F. Buchli Mission Specialist 3 Robert C. Springer Payload Specialist 1 Nigel Wood United Kingdom Payload Specialist 2 Pratiwi Sudarmono Indonesia Backup crew Payload Specialist 1 Richard Farrimond United Kingdom Payload Specialist 2 Taufik Akbar Indonesia Mission objectives The main task of the mission was to bring three commercial satellites into orbit Skynet satellites Skynet 4A , Palapa B3 and Westar 6S. The British Skynet and the Indonesia n Palapa were supposed to be accompanied by an astronaut from the two countries. After the Space Shuttle Challenger disaster Challenger disaster the deployment of commercial satellites by the Space Shuttle was stopped, also for several years no international astronauts were nominated anymore. Thus neither the British nor the Indonesian payload specialists got a second chance for a spaceflight. The NASA crew however stayed together and finally flew on STS 29 , only Anna Fisher was replaced by James Bagian on that flight. Skynet 4A was launched on 1 January 1990 with a Titan III , Westar 6S was renamed Galaxy 6 and launched on 12 October 1992 by an Ariane 4 Ariane 44L . Palapa B3 was renamed to Palapa B2P and was launched on 20 March 1987 with a Delta rocket Delta 3920 . See also Cancelled Shuttle missions STS 61 M External links http www.mach25.nl jacques shuttle STS61H.html Space Shuttle Columbia DEFAULTSORT STS 061 H Category Cancelled Space Shuttle missions nl STS 61 H ja STS 61 H pl STS 61 H pt STS 61 H ... more details
In packet switched packet switched computer networks, a jumbogram portmanteau of jumbo disambiguation jumbo and datagram is an internet layer packet exceeding the standard Maximum Transmission Unit MTU of the underlying network technology. Large packets for link layer technologies are referred to as jumbo frame s. The payload length field of IPv4 and IPv6 has a size of 16 bits, thus allowing data of up to gaps 65 535 octets . This theoretical limit for the Internet Protocol IP MTU, however, is reached only on networks that have a suitable Link Layer infrastructure. While IPv4 has no facilities to exceed its theoretical IP MTU limit, the designers of IPv6 have provided a protocol extension to permit packets of larger size. Thus, in the context of IPv6 a jumbogram is understood as an IPv6 packet carrying a Payload computing payload larger than gaps 65 535 octet computing octet s ref name rfc2675 Borman, D. Steve Deering Deering, S. Hinden, R. August 1999 . http tools.ietf.org html rfc2675 IPv6 Jumbograms . Internet Engineering Task Force IETF . RFC nbsp 2675. ref IPv6 jumbograms An optional feature of IPv6, the jumbo payload option, allows the exchange of packets with payloads of up to one byte less than 4 GiB 2 sup 32 sup 1 4,294,967,295 bytes , by making use of a 32 bit length field. Historically, Transport Layer protocols, such as the Transmission Control Protocol TCP and the User Datagram Protocol UDP , include data size parameters limited to only 16 bits length, urgent data pointer . The support for IPv6 jumbograms required a redesign in all Transport Layer protocols. The jumbo payload option and the transport layer modifications are described in RFC 2675. References Reflist Category Packets information technology Category IPv6 fr Jumbogram ... more details
The NASA Space grant colleges SpaceGrant Consortium at the University of Colorado at Boulder has sponsored many small space reaching missions including 3CS, CX, DINO, DANDE , and RocketSat . RocketSat is a small payload which launched on a sounding rocket provided by the UP Aerospace corporation in October 2006. It is interesting to note that this first launch for the University of Colorado RocketSat program also marks the nascent flight of the UP Aerospace corporation, and the inaugural launch for the Southwest Regional Spaceport near Upham, New Mexico. Purpose RocketSat was conceived as the framework for a sister class to the BalloonSat projects course Gateway to Space , already offered to freshman engineering students at the University of Colorado at Boulder University of Colorado . The first RocketSat Payload air and space craft payload serves as the proof of concept for future classes. This original payload consists of various instrumentation to record Geiger counter Geiger radiation counts, microwave radiation intensity, pressure , temperature , and acceleration on three axes in both high range with low precision and low range with high precision. An I C EEPROM and two linked BrainStems tm via the I2C bus are used to record the myriad of data collected by the sensors. Due to the limited BrainStem speed, and limited EEPROM storage space, the data collected on this RocketSat flight is being recorded at 4 Hertz . Gallery Image RSLogo.jpg The RocketSat logo Image RocketSat1.jpg Fully assembled RocketSat payload Image RocketSat2.jpg Accelerometer board close up External links http Brandon.Gilles.GooglePages.com Photos of RocketSat http rocketsat.googlepages.com home RocketSat website http spacegrant.colorado.edu Colorado SpaceGrant Consortium Category NASA programs Category University of Colorado at Boulder ... more details
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