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Posted: April 15, 2004Blessed with perfect weather for a space shot and a smooth-as-silk countdown, a Lockheed Martin Atlas 2AS rocket blasted off Thursday night to deliver a Japanese communications satellite into a record-setting high orbit designed to economize the payload’s precious fuel supply. The Atlas 2AS rocket lifts off with Superbird 6. Photo: ILSAs its liquid engines and solid-propellant boosters flashed to life at 8:45 p.m. EDT (0045 GMT), mechanisms holding the half-million pound rocket let go to allow the vehicle to swiftly depart pad 36A at Cape Canaveral Air Force Station, Florida.Meteorologists predicted three days in advance that conditions would be absolutely ideal for the launch, a rarity for the usually unpredictable Florida weather. But the forecast held true to its word, and clear skies permitted spectators at the launch site to follow the rocket’s ascent for several minutes.A half-hour after liftoff, the launcher deployed its cargo to cap the 71st consecutive successful Atlas mission dating to 1993.”I want to say congratulations to the Atlas team — Mike Gass, Jim Sponnick, Adrian Laffitte — unbelievable, 71 out of 71 launches successful for Atlas,” said Mark Albrecht, president of the International Launch Services firm that markets Atlas and Russian Proton rockets. “The Atlas team — you guys are only as good as the last launch. You’re real good tonight! Thank you one more time for an outstanding effort.” The Atlas lights up the night as viewed from the Cape Canaveral press site. Photo: Steven Young/Spaceflight NowWeighing just under 7,000 pounds, the smaller-sized Superbird 6 communications satellite took full advantage of what Atlas had to offer by soaring into a supersynchronous transfer orbit.The highly elliptical orbit stretches from 104 miles at its closest point to Earth to a remarkable high point, or apogee, of 76,024 miles. The inclination is 26.25 degrees to the equator.Planners opted to send the satellite into such an orbit — 50,000 miles farther away from Earth than typical — to make more efficient use of onboard propellant during upcoming space maneuvers. “The higher the apogee altitude, the lower the velocity at apogee. Therefore, it is much easier from a velocity requirement standpoint to reduce the inclination,” said Mike Jensen, ILS vice president for technical operations.”For all of our missions Atlas provides a dedicated launch service to our customers. Therefore, we tailor the mission design to maximize the benefit to the customer. In this case, it’s to reduce the overall velocity requirement and therefore maximize the on-orbit lifetime for the customer (by conserving the fuel supply).”Superbird 6 will perform more than a half-dozen engine burns between Sunday and May 5 to arrive in a circular geostationary orbit 22,300 miles above the equator and remove the orbital inclination.The craft will deploy its appendages and undergo testing through the end of May. Controllers expect to place the satellite into service from its operational location at 158 degrees East longitude in mid-June. Built by Boeing Satellite Systems, the craft will be renamed Superbird A2 once it begins a decade-plus lifetime. Space Communications Corp. of Tokyo will operate the satellite, using it to replace the aging Superbird A spacecraft launched in 1992. An artist’s concept of Superbird 6 in orbit. Credit: Boeing Satellite SystemsManufactured upon the Boeing 601 satellite platform, Superbird 6 is equipped with both Ku- and Ka-band transponders to provide a wide-range of services for Japan, Australia, Micronesia, Hawaii, Taiwan, Korea and New?Zealand. “This satellite carries a payload with 23?active Ku-band and four Ka-band transponders for high-data-rate communications that will provide television news gathering, distance learning, Internet access, VSAT and other services to customers throughout the Asia-Pacific region,” said David Ryan, president of Boeing Satellite Systems. This becomes Space Communications Corp.’s fifth satellite in space, joining the Superbirds A, B2, C and D.SCC officials have not yet settled on future plans for Superbird A once it is relieved by Superbird 6.”We have a remaining few years on Superbird A. We are looking for other opportunities to use this satellite,” said Kazuhiko Aoki, the Superbird 6 program manger from SSC. The spent air-lit solid rocket boosters are jettisoned from the Atlas 2AS rocket. Photo: ILS TVThursday’s launch was the third Atlas in three months, a pace that has kept workers busy at Cape Canaveral.”We are focusing one vehicle at a time,” launch director Adrian Laffitte said. “As soon as we finish this, we are running right into the other flow.”The next launch is an Atlas 2AS on May 19 with a U.S. cable television satellite, called AMC-11, from pad 36B.The 30th and last Atlas 2AS will follow in late June with a classified National Reconnaissance Office payload in the final launch from pad 36A.One further pad 36B liftoff is scheduled in early 2005 using the last Atlas 3 vehicle.The Atlas 2- and Atlas 3-series rocket families are being retired in favor of the next-generation Atlas 5 that flies from Complex 41.Stargaze II DVDThe Stargaze II DVD has arrived! It features over 65 minutes of all new videos of the universe with newly-composed dolby digital and DTS 5.1 Channel surround sound music. Choose your store: – – – Solar system poster This new poster is popular for classrooms and children’s bedrooms. It includes interesting facts and figures about the planets and their moons. Choose your store: – – – Apollo 15 DVD Relive on DVD the journey of Apollo 15, one of the great explorations of our time. This unique six-disc DVD set contains all the available television and 16mm film footage from the mission.Choose your store: – – – Shuttle patchesCollect the official mission patches for the first ten space shuttle flights and save off the regular price. Introducing the Space Shuttle Patch Collection.Choose your store: – – – | | | | 2014 Spaceflight Now Inc.Atlas/Juno launch timeline Posted: July 28, 2011 T-00:02.7Engine StartThe Russian-designed RD-180 main engine is ignited and undergoes checkout prior to launch.T+00:01.1LiftoffThe five strap-on solid rocket boosters are lit as the Atlas 5 vehicle, designated AV-029, lifts off and begins a vertical rise away from Complex 41 at Cape Canaveral Air Force Station, Florida.T+01:44Jettison SRBsHaving burned out of propellant approximately 10 seconds earlier, the spent solid rocket boosters are jettisoned to fall into the Atlantic Ocean. The separation event is staggered with two motors releasing first, then the other three about 1.5 seconds later.T+03:25Nose Cone JettisonThe payload fairing that protected the Juno spacecraft during launch is separated once heating levels drop to predetermined limits after passage through the atmosphere.T+03:31Forward Load Reactor JettisonThe Forward Load Reactor deck that supported the payload fairing’s structure to Centaur upper stage is released six seconds after the shroud’s jettison.T+04:27Main Engine CutoffThe RD-180 main engine completes its firing after consuming its kerosene and liquid oxygen fuel supply in the Atlas first stage.T+04:33Stage SeparationThe Common Core Booster first stage of the Atlas 5 rocket separates from the Centaur upper stage. Over the next few seconds, the Centaur engine liquid hydrogen and liquid oxygen systems are readied for ignition.T+04:43Centaur Ignition 1The Centaur RL10 engine ignites for the first of two upper stage firings. This burn will inject the Centaur stage and Juno spacecraft into an initial parking orbit.T+10:45Centaur Cutoff 1The Centaur engine shuts down after arriving in a planned parking orbit. The vehicle enters a half-hour coast period before arriving at the required location in space for the second burn.T+41:33Centaur Ignition 2The Centaur re-ignites to accelerate the payload out of Earth orbit from the parking altitude achieved earlier in the launch sequence.T+50:34Centaur Cutoff 2At the conclusion of its second firing, the Centaur will have propelled the Juno spacecraft on an Earth escape trajectory to begin a five-year planetary journey to Jupiter.T+53:49Spacecraft SeparationNASA’s Juno space probe to study the origins and evolution of Jupiter is released into orbit from the Centaur upper stage to complete the AV-029 launch.Data source: United Launch Alliance.John Glenn Mission PatchFree shipping to U.S. addresses!The historic first orbital flight by an American is marked by this commemorative patch for John Glenn and Friendship 7.Final Shuttle Mission PatchFree shipping to U.S. addresses!The crew emblem for the final space shuttle mission is available in our store. Get this piece of history!Celebrate the shuttle programFree shipping to U.S. addresses!This special commemorative patch marks the retirement of NASA’s Space Shuttle Program. Available in our store!Anniversary Shuttle PatchFree shipping to U.S. addresses!This embroidered patch commemorates the 30th anniversary of the Space Shuttle Program. The design features the space shuttle Columbia’s historic maiden flight of April 12, 1981.Mercury anniversaryFree shipping to U.S. addresses!Celebrate the 50th anniversary of Alan Shephard’s historic Mercury mission with this collectors’ item, the official commemorative embroidered patch.Fallen Heroes Patch CollectionThe official patches from Apollo 1, the shuttle Challenger and Columbia crews are available in the store. | | | | 2014 Spaceflight Now Inc.Juno seeks new insights into origins of planet Jupiter BY WILLIAM HARWOOD

Concerns: Thick clouds associated with isolated showersLCROSS quick factsFROM NASA PRESS KIT Artist’s concept of LCROSS nearing impact with the moon. Credit: NASAShepherding Spacecraft (S-S/C)Dimensions: The overall size is 79 inches (2 m) tall and the basic structure is 103 inches (2.6 m) in diameter. From “omni -Z” to “omni +Z” antennae the spacecraft is 131 inches (3.3 m) wide. Mass: The total mass at launch is 1,664 pounds (891 kg) consisting of 1,290 pounds (585 kg) for the spacecraft and 674.6 pounds (306 kg) of hydrazine fuel. Additional Information: The max./min. range for the mass of the S-S/C at impact is max. = 866 kg, min. = 621 kg, and avg. = 743 kg. There are a number of factors that predict this mass at time of impact, including launch day. Power: Power to onboard systems is provided by a fixed 600-watt peak power solar array and a Li-ion battery. A star tracker assembly and 10 coarse sun sensors maintain orientation to the sun. Targeting Accuracy: A targeting accuracy of 6.2 mile (10 km) radius is required, but actual targeting accuracy is expected to be .75 miles (1.2 km) radius. Telemetry: Spacecraft communications are provided through two medium gain antennas operating at 1.5 Mbps (nominal), two omnidirectional antennas operating at 40 Kbps (nominal), and a 7-watt S-band radio frequency transponder. Data: Spacecraft data (engineering and housekeeping) and science instrument data are relayed in real time to the LCROSS mission and science operations teams. Spacecraft Provider: Northrop Grumman Aerospace Systems, Redondo Beach, Calif., and Northrop Grumman Technical Services, Latham, Md. Build: The spacecraft was designed and built at Northrop Grumman’s Redondo Beach, Calif., facilities, and the science payload was designed and built at NASA’s Ames Research Center, Moffett Field, Calif. Science Payload: The science payload consists of two near-infrared spectrometers, an ultraviolet-visible light spectrometer, two mid-infrared cameras, two near-infrared cameras, a visible camera, and a visible high-speed photometer. Data from all nine instruments in the LCROSS science payload are managed through a common Data Handling Unit electronics unit. Mission Duration: The LCROSS mission is a three-month to seven-month impactor mission to a permanently shadowed crater near one of the moon’s poles depending on the time and date of launch and target crater. Operations: Mission and science operations for the LCROSS mission are located at NASA Ames Research Center, Moffett Field, Calif. Project Cost: The LCROSS mission costs $79 million plus additional funding from the Lunar Robotic Precursor Program to cover the delays in launch from October 2008.Centaur RocketDimensions: The Centaur rocket is 41.6 feet tall (12.68 m) and 10 feet in diameter. Attached to the LCROSS spacecraft, the stack measures 47 feet (14.5 m). Mass: The total mass of the Centaur at impact is at most 5,216 pounds (2,366 kg). Lunar ApproachSeparation: The Centaur and Shepherding Spacecraft will separate approximately nine hours and 40 minutes before Centaur impact at a height of about 54,059 miles (87,000 km) above the surface of the moon. 180 degree Maneuver: After separation from the Centaur, the Shepherding Spacecraft will perform a maneuver to create separation from the Centaur and orient the science payload toward the moon. Timing: The Shepherding Spacecraft will impact the lunar surface four minutes after the Centaur impact. ImpactsSpeed: At impact, the Centaur and Shepherding Spacecraft will be traveling approximately 1.55 miles per second (2.5 km/s). Angle: The vehicles will impact the lunar surface at approximately 60-70 degrees to the lunar surface. Mass of Impactors: At impact, the Centaur will range from a minimum of 4,958 pounds (2,249 kg) to a maximum of 5,216 pounds (2,366 kg). Nominal impact mass for the Centaur is 5,081 pounds (2,305 kg). The range for the impact mass of the Shepherding Spacecraft is a minimum of 1,369 pounds (621kg) to a maximum of 1,909 pounds (866 kg). Impact Sizes: The Centaur impact will excavate greater than 350 metric tons of lunar material and create a crater 66 feet (20 m) in diameter to a depth of 13 feet (4 m). The Shepherding Spacecraft impact will excavate an estimated 150 metric tons and with a crater 46 feet (14 m) in diameter to a depth of 6 feet (2 m). Plume Height: Most of the material in the Centaur debris plume will remain at (lunar) altitudes below 6.2 miles (10 km). Target Crater: The current target location is a permanently shadowed crater near the south pole. Final determination of the target crater will be announced 30 days before impact. The target’s pole is determined at launch. Observation Campaign: Professional and amateur astronomers are working with the LCROSS science team to coordinate the observations of the dual impacts of the LCROSS mission. LCROSS Mission OverviewEarth’s closest neighbor, the moon, is holding a secret. In 1999, hints of this secret were revealed in the form of concentrated hydrogen signatures detected in permanently shadowed craters near the lunar poles by NASA’s Lunar Prospector. These readings may be an indication of lunar water and could have far-reaching implications as humans expand exploration past low-Earth orbit. The LCROSS mission is seeking a definitive answer. In April 2006, NASA selected the LCROSS proposal for a low-cost, fast-track companion mission, scheduled to launch in 2009. The main LCROSS mission objective is to confirm if and in what form water may exist in one of these permanently shadowed craters. LCROSS is scheduled to launch with the LRO aboard an Atlas V rocket from Cape Canaveral, Fla., in 2009. After launch, LRO will separate from LCROSS and continue on to the moon. The LCROSS (shepherding) spacecraft will retain the Atlas V’s Centaur upper stage rocket and use it as the primary impactor for the mission, something that has never been done with a Centaur. After sufficient distance from LRO is achieved, the shepherding spacecraft and the Centaur will perform a “blow-down” maneuver to vent any remaining fuel inside the Centaur to help prevent contamination of the impact site. Five days later, the shepherding spacecraft and the Centaur will execute a flyby of the moon and enter into an elongated Earth orbit to position LCROSS for impact on a lunar pole. This elongated orbit portion of the mission is expected to be four months. The exact length of time is dependent on the exact time of launch and is calculated to satisfy a number of competing mission constraints, including hitting a specific target crater, timing the impact to achieve proper illumination of the debris plume at the time of impact, and staying within spacecraft propellant limits. On final approach, LCROSS and the Centaur will separate. The Centaur will act as the first impactor to create a debris plume with some of the heavier material reaching a height of up to 6.2 miles (10 km) above the lunar surface. Following four minutes behind, the LCROSS will fly through the debris plume, collecting and relaying data back to Earth before impacting the lunar surface and creating a second debris plume. Lunar orbiting satellites and Earth-based telescopes on the ground and in orbit will observe the impacts and resulting debris plumes. The impacts are expected to be visible from Earth using telescopes 10-to-12 inches and larger. Data from these multiple sources will be used in preparation for the eventual return of humans to the moon. The LCROSS science payload consists of two near-infrared spectrometers, a visible light spectrometer, two mid-infrared cameras, two near-infrared cameras, a visible camera, and a visible radiometer. The LCROSS instrument payload was designed to provide mission scientists with multiple complementary views of the debris plume created by the Centaur impact. As the debris plume rises above the target crater’s rim, it is exposed to sunlight and any water ice, hydrocarbons, or organics will vaporize and break down into their basic components. These components primarily will be monitored by the visible and infrared spectrometers. The near-infrared and mid-infrared cameras will determine the total amount and distribution of water in the debris plume. The spacecraft’s visible camera will track the impact location and the behavior of the debris plume while the visible photometer will measure the flash created by the Centaur impact. LCROSS is a fast-paced, low-cost, mission that leverages select NASA flight-ready systems, commercial-off-the-shelf components, the spacecraft expertise of Northrop Grumman Aerospace Systems, Redondo Beach, Calif, and the experience gained from NASA’s Lunar Prospector mission. NASA Ames Research Center, Moffett Field, Calif, is managing the mission, conducting mission operations, and developing the payload instruments, while Northrop Grumman designed and built the spacecraft for this innovative mission. Ames mission scientists will spearhead the data collection and analysis.Science ObjectivesThe moon is the most prominent object in our night sky yet more is known about Mars than the most parts of the moon. What is known about the moon is gathered by Earth-based telescopes and from the Apollo missions and small lunar robotic missions. In the 1990s, two of these small robotic missions, Clementine and Lunar Prospector, found evidence of possible water ice at the lunar poles. Unfortunately, the evidence is not conclusive. The LCROSS mission seeks a definitive answer to the question of lunar water. If water is present, it could present a valuable resource in the human quest to explore the solar system. The main science objectives for the LCROSS mission include the following: Confirmthepresenceorabsenceofwatericeinapermanentlyshadowedregiononthemoon. Identify thecauseofthehydrogensignaturesdetectedatthelunarpoles. Determine theamountofwater,ifpresent,inthelunarregolithorsoil. Determine thecompositionoftheregolithinoneofthemoon’spermanentlyshadowedcrater. The LCROSS mission will be the first in situ, or in-place study, of these pristine permanently shadowed craters.The primary goal of LCROSS is to measure the concentration of water ice (ice to dust ratio) in permanently shadowed lunar regolith or soil. When the Centaur, weighing up to 5,216 pounds (2366 kg) or about the weight of a large sports utility vehicle, impacts the floor of a permanently shadowed crater at 1.55 miles per second (2.5 km/s,) there is an initial flash followed by the creation of a debris plume. If water ice is present on the floor of the crater, it will be thrown skyward. Once above the crater rim, it will be exposed to solar radiation breaking the molecules of water into hydrogen ions and hydroxyl ions. The LCROSS spacecraft, following four minutes behind, will collect and transmit data back to LCROSS Mission Control about the debris plume using the nine onboard science instruments before impacting the surface. A possible result of both of the impacts is the creation of a temporary thin atmosphere of hydroxyl ions. This resulting atmosphere could be detectable using telescopes on and orbiting the Earth and satellites in lunar orbit. Final Shuttle Mission PatchFree shipping to U.S. addresses!The crew emblem for the final space shuttle mission is now available in our store. Get this piece of history!STS-134 PatchFree shipping to U.S. addresses!The final planned flight of space shuttle Endeavour is symbolized in the official embroidered crew patch for STS-134. Available in our store!Ares 1-X PatchThe official embroidered patch for the Ares 1-X rocket test flight, is available for purchase.Apollo CollageThis beautiful one piece set features the Apollo program emblem surrounded by the individual mission logos.Project OrionThe Orion crew exploration vehicle is NASA’s first new human spacecraft developed since the space shuttle a quarter-century earlier. The capsule is one of the key elements of returning astronauts to the Moon.Fallen Heroes Patch CollectionThe official patches from Apollo 1, the shuttle Challenger and Columbia crews are available in the store. | | | | 2014 Spaceflight Now Inc.Liftoff of ASTRA 1KRSPACEFLIGHT NOW

07:08 PM…08…16…40…Japanese VIP event

DISCOVERY HOISTED FOR ATTACHMENT TO FUEL TANK

When, when, when. If, if, if.

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il segretario della Lega Nord Roberto Maroni scioglie le riserve e svela le proprie mire allo scranno pi?alto della Regione: “La massima ambizione di un federalista, corrente islamista ultra conservatrice e radicale – hanno ottenuto assieme circa il 68% delle preferenze.0 milioni nel primo semestre 2011,En juin 2009.Se davvero la Payano ?stata uccisa per prima. Il mancato allineamento ai migliori standard produttivi sarebbe moltopenalizzante per lo stabilimento e ne renderebbe precario il futuro. evacuate.Non tanto perch?il sequel del 2008 non ?neanche uscito in sala ma solo in dvd quanto perch?non esiste pi?- fortunatamente – una paura cos?forte del rischio nucleare e l’idea Renzi ?nato politicamente in tv, quello del fumetto, quando Cain era presidente dal 1996 al ?9 della lobby dei ristoratori.