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Av Clio Mob.Pdf ATLAS V Pantone 661 Pantone Black 6 A United Launch Alliance Atlas V 401 launch vehicle will deliver Pantone 459 the CLIO spacecraft to orbit for Lockheed Martin Space Systems Company. Liftoff will occur from Space Launch Complex 41 at Cape Canaveral Air Force Station, FL. Pantone Cool Gray 10 Pantone 286 Since 1957, the Atlas rocket has been an integral part of the United The ULA team is proud to launch the CLIO mission on an Atlas V 401, States’ space program, supporting national defense missions, from Space Launch Complex 41, for Lockheed Martin Space Systems launching Mercury astronauts to orbit, and sending spacecraft to the Company. farthest reaches of the solar system. Over its nearly six decades, the The ULA team is focused on attaining Perfect Product Delivery for the Atlas booster has undergone a series of continuous improvements, CLIO mission, which includes a relentless focus on mission success (the culminating in the current Atlas V Evolved Expendable Launch Vehicle perfect product) and also excellence and continuous improvement in (EELV). Designed in partnership with the U.S. Air Force, the modu- meeting all of the needs of our customers (the perfect delivery). lar design of the Atlas V allows for multiple configurations to meet specific customer requirements. We sincerely thank the entire team, which consists of Lockheed Martin, their U.S. government sponsor, ULA, and major suppliers of ULA. All Atlas V launch vehicles consist of a common core booster first stage, a Centaur second Go Atlas, Go Centaur, Go CLIO! stage, and either a 4-m-diameter or a 5-m-diameter payload fairing. To accommodate larger spacecraft requiring additional thrust at liftoff, one to three solid rocket boosters (SRB) can be added to the Atlas V 4-m vehicle, while the Atlas V 5-m vehicle can support up to five SRBs. Flexibility, reliability and 100% mission success are the hallmarks of the Atlas V system, Jim Sponnick making it the launch vehicle of choice for the full range of customer requirements. Vice President, Atlas and Delta Programs Payload Fairing (PLF) The CLIO spacecraft is encapsulated in the 4-m (14-ft) diameter large payload fairing (LPF). The LPF is a bisector (two-piece shell) fairing consisting of aluminum skin/stringer construction with vertical split-line longerons. The vehicle’s height with the PLF is approximately 189 ft. Centaur The Centaur second stage is 10 ft in diameter and 41.5 ft in length. Its propellant tanks are constructed MISSION OVERVIEW of pressure-stabilized, corrosion resistant stainless steel. Centaur is a liquid hydrogen/liquid oxygen- (cryogenic-) fueled vehicle. It uses a single RL10A-4-2 engine producing 22,300 lb of thrust. The cryo- genic tanks are insulated with a combination of helium-purged insulation blankets, radiation shields, and spray-on foam insulation (SOFI). The Centaur forward adapter (CFA) provides the structural mountings for PMS 280C PMS 279C PMS 123C Black With more than a century of combined heritage, United Launch Alliance is – 25th Atlas V 401 Configuration Launch the fault-tolerant avionics system and the structural and electrical interfaces with the spacecraft. the nation’s most experienced and reliable launch service provider. ULA th has successfully delivered more than 85 satellites to orbit that provide – 49 Atlas V Launch Booster critical capabilities for troops in the field, aid meteorologists in tracking – 60th ULA Launch from Cape Canaveral The Atlas V booster is 12.5 ft in diameter and 106.5 ft in length. The booster’s tanks are structurally rig- severe weather, enable personal device-based GPS navigation and unlock id and constructed of isogrid aluminum barrels, spun-formed aluminum domes, and intertank skirts. Atlas the mysteries of our solar system. – 88th Overall ULA Launch booster propulsion is provided by the RD-180 engine system (a single engine with two thrust chambers). The RD-180 burns RP-1 (Rocket Propellant-1 or highly purified kerosene) and liquid oxygen, and deliv- ers 860,200 lb of thrust at sea level. The Atlas V booster is controlled by the Centaur avionics system, which provides guidance, flight control, and vehicle sequencing functions during the booster and Centaur Join the conversation: phases of flight. Bringing Rocket Science Down to Earth. ULALaunch.com Copyright © 2014 United Launch Alliance, LLC. All Rights Reserved. PMS 280C PMS 279C PMS 123C Black ATLAS V PRODUCTION AND LAUNCH MISSION PROFILE AND GROUND TRACE 1 De Denver, Soto, CO CA • RS-68 Engine Fabrication at Aerojet Rocketdyne 1 De– ULA Soto, Headquarters CA & Design 6 7 8 9 2 2 Brigham• CenterRS-68 EngineeringEngine City ,F abricationUT at Aerojet Rocketdyne • Solid Rocket Motor Fabrication at Alliant Technologies 5 2 3 21 DeBrighamHarlingen, Soto, TXCACity, UT 13 Denver•De– SolidRS-68Payload Soto, Rocket ,Engine Fairing,CO CA Motor F Payloadabrication Fabrication Fairing at Aerojet at Alliant Rocketdyne Technologies 1 3 De• RS-68 Soto, Engine CA Fabrication at Aerojet Rocketdyne 21 Brigham• Adapter,ULARS-68 Headquarters Engine Booster City ,F abrication UTAdapter & Design & at Centaur AerojetCenter EngineeringRocketdyne 4 2 23 •BrighamDenver RS-68 ,Engine CO City ,F abricationUT at Aerojet Rocketdyne 1 4 2 •Brigham Adapter Fabrication City, UT 2 • SolidULA HeadquartersRocket Motor & F abricationDesign Center at Alliant Engineering Technologies 2 3 4 24 •BrighamDecatur Solid Rocket, ALCity Motor, UT Fabrication at Alliant Technologies Time Time 3 3 DenverDecatur, ,AL CO Event (seconds) (hr:min:sec) 1 3 43 DecaturDenver• SolidPayload Rocket, ,FCO ALairing/Adapter Motor Fabrication Fabrication at Alliant Technologies 1 3 3 •Denver– Booster, FabricationCO & Final Assembly, 1 4 5 • ULAPBoosterayload Headquarters Fabricationairing/Adapter & Design Fabrication Center Engineering 1 RD-180 Engine Ignition -2.7 -00:00:02.7 1 4 3 •Denver CentaurSecondULA Headquarters, TankStageCO Fabrication Fabrication & Design & Centaur Center Engineering 4 5 4 •Decatur ULABooster Headquarters ,F ALabrication & Design Center Engineering Liftoff (Thrust to Weight > 1) 1.1 00:00:01.1 4 4 Decatur• FinalSecond Assembly ,Stage AL Fabrication 5 W• Pestayload Palm Fairing/Adapter Beach, FL Fabrication Begin Pitch/Yaw Maneuver 17.5 00:00:17.5 4 •DecaturWest BoosterPayload Palm ,F ALabricationairing/AdapterBeach, FL Fabrication 5 • RL10Booster Engine Fabrication Fabrication at Aerojet Rocketdyne 5 5 •W– SecondBoosterPRL10estayload P Enginealm StageFabricationairing/Adapter Beach, Fabrication Fabrication FL F atabrication Aerojet Mach 1 79.1 00:01:19.1 • BoosterRL10Second Engine StageFabrication F Fabricationabrication at Aerojet Rocketdyne 5 • RocketdyneSecond Stage Fabrication 3 Maximum Dynamic Pressure 90.9 00:01:30.9 5 • Second Stage Fabrication 5 WKhimki,est P Russiaalm Beach, FL 5 •W RL10est P Enginealm Beach, Fabrication FL at Aerojet Rocketdyne 2 Atlas Booster Engine Cutoff (BECO) 241.8 00:04:01.8 •– RL10RD-180 Engine Engine Fabrication Fabrication at atAerojet Rocketdyne 5 •W RL10est P Enginealm Beach, Fabrication FL at Aerojet Rocketdyne 3 Atlas Booster/Centaur Separation 247.8 00:04:07.8 • NPORL10 Energomash Engine Fabrication at Aerojet Rocketdyne 4 Centaur Main Engine Start (MES-1) 257.8 00:04:17.8 5 Payload Fairing Jettison 265.8 00:04:25.8 1 Atlas Spaceflight Operations Center (ASOC) | Launch 6 Centaur First Main Engine Cutoff (MECO-1) 1,078.1 0:17:58.1 Control Center and Mission Director’s Center 7 Centaur Second Main Engine Start (MES-2) 10,072.9 2:47:52.9 2 Spacecraft Processing Facility | Spacecraft processing, 1 Vertical Integration Facility (VIF) testing and encapsulation (See inset) 8 Centaur Second Main Engine Cutoff (MECO-2) 10,143.3 2:49:03.3 3 2 Bridge Crane Hammerhead 2 9 CLIO Separation 10,312.3 2:51:52.3 Vertical Integration Facility | Launch vehicle Integration 3 and testing, spacecraft mate and integrated operations 3 Bridge Crane Interstage 4 Launch Vehicle Adapter Interstage 2 Adapter Booster 5 Mobile Launch Platform (MLP) Longitude (deg) 6 Centaur LO Storage 2 4 7 High Pressure Gas Storage 5 80 1 Centaur 8 Booster LO Storage 2 5 60 9 Pad Equipment Building (PEB) 10 Pad ECS Shelter 40 TEL-4 4 JDMTA 20 6 (deg) TDRS Spacecraft Guam 4-m Payload 171 Fairing Halves 0 TDRS 041 TDRS 046 Diego Garcia 9 TDRS 1 174 Payload -20 Geodetic Latitude Transporter 8 7 1 -40 4 -60 Telemetry Ground Station 2 10 Launch Vehicle /Spacecraft Ground Trace TDRS Asset Geostationary Orbital Position 3 6 -80 45 Mobile 7 8 -135 -90 -45 0 90 135 Launch Space Launch Complex 41 Platform 9 All Values Approximate.
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