launchsystem or reusablelaunch vehicle , RLV is a launchsystem which is capable of launching a launch vehicle into space more than once. This contrasts with expendable launchsystem s, where each launch vehicle is launched once and then discarded. No true Orbital spaceflight orbital reusablelaunchsystem is currently in use. The closest example is the partially reusable Space Shuttle ... launchsystem for small payloads Historical Space Shuttle partially reusable, retired Soviet Union ... proposed reusable European launchsystem HOTOL British SSTO Hyperion SSTO 1960s concept HTVL spacecraft ... often depicted space launch vehicles as either single stage reusable Destination Moon film rocketships which could launch and land vertically SSTO VTVL , or single stage reusable rocketplanes which ... feasible. Before VTVL SSTO designs came the partially reusable multi stage NEXUS launch vehicle NEXUS ... designs to reduce vehicle structural mass. Use of in flight refueling. Other launchsystem configuration ... the HL 20 Personnel LaunchSystem HL 20 and Orbital Sciences X 34 X 34 are examples from the 1990s ... to be expensive to maintain, even more expensive than an expendable launchsystem would have been. The cancellation ... even before that, due to unresponsiveness to customer concerns by the Shuttle launchsystem. In 1986 ... demonstrated it was possible to make a reusable space launch vehicle which did not require a large .... This fueled a private launch industry, including partially reusable vehicle players, such as Kistler ... incentive. SpaceX is a recent player in the private launch market which has partially reusable vehicles ... these materials for a reusablelaunch vehicle, whose raison d etre is high flight rates for economical launch costs. Weight penalty The weight of a reusable vehicle is almost invariably higher than an expendable .... Maintenance Reusablelaunch systems require maintenance, which is often substantial. The Space .... Streamlining the manpower requirements of any launchsystem is an essential part of making ... more details
The Reusable Booster System RBS is a United States Air Force circa 2010 program to develop a new VTHL vertical takeoff, horizontal landing VTHL ref name dbj20110322 reusable booster and a new expendable second stage to replace the existing Evolved Expendable Launch Vehicle s EELV after 2025. ref name rlvst20100920 cite news title Air Force studying reusable upper stage systems for reusable booster url http hobbyspace.com nucleus index.php?itemid 23692 accessdate 2011 03 24 newspaper RLV and Space Transport News date 2010 09 20 ref Program description Program funding is set at currency 250000000 US . ref name dbj20110322 Officials anticipate awarding up to three contracts for the project, where winners would compete for individual tasks of experiments and demonstrations that address technology, processes and other attributes of a reusable booster system, or RBS. The proposal deadline is 19 March 2011. ref name dbj20110322 cite news last Cogliano title Air Force launches 250M reusable booster initiative url http www.bizjournals.com dayton news 2011 03 22 air force launches 250m reusable.html accessdate 2011 03 24 newspaper Dayton Business Journal date 2011 03 22 quote Officials anticipate awarding up to three contracts for the project, where winners would compete for individual tasks of experiments and demonstrations that address technology, processes and other attributes of a reusable booster system, or RBS. Air Force officials envision an RBS that includes a reusable rocket and an expendable upper stage rocket. The reusable rocket would be launched vertically and return, landing ... Martin Selected USAF for Reusable Booster System Flight Demonstrator Program 999.html ref See also ... Reusable Booster System Study Contract , RLV and Space Transport News, September 2010. Category Unmanned ... Reusable Booster Ideas , Aviation Week , May 14, 2009 http hobbyspace.com nucleus index.php?itemid 23692 Air Force studying reusable upper stage systems for reusable booster , RLV and Space Transport ... more details
Canaveral Air Force Station Space Launch Complex 17 CCAFS SLC 17 An expendable launchsystem is a launch vehicle launchsystem that uses an expendable launch vehicle ELV to carry a payload into space . The vehicles used in expendable launch systems are designed to be used only once i.e. they are expended during a single flight , and their components are not recovered for re use after launch. The vehicle ... gains altitude and speed. Design rationale The ELV design differs from that of reusablelaunchsystem s, where the vehicle is launched and recovered more than once. Reuse might seem to make ... the Shuttle, is the only existing launch vehicle that is even partly reusable. but in practice ... to a reusablesystem whose weight, supplies and life support systems further decrease payload ... Spaceflight DEFAULTSORT Expendable LaunchSystem Category Spacecraft propulsion Category Space ... failure, a short time to launch and a relatively low cost. Who date January 2009 Can someone expand ... to launch as much payload per unit of gross liftoff weight due to the mass fraction advantages ... in their design. A prime example of this is the Titan IV , probably the costliest per unit launch vehicle in history perhaps following the Space Shuttle . On the other hand, a reusable launcher such as the Shuttle requires a heavier structure and a recovery system wings, thermal protection system ... launch vehicle and presence of a crew require stringent man rated flight safety precautions that increase launch and payload costs. Only five orbiters were built, and the unexpected loss of two ... flights compared to that following most expendable launch failures, each of which impacted only ... family. By 1995 Arianespace lofted its 100th satellite and by 1997 the Ariane rocket had its 100th launch ... of the United States that NASA be the public sector provider of U.S. launch capacity ... States President Ronald Reagan signed into law the Commercial Space Launch Act. ref http www.reagan.utexas.edu ... more details
Image Nls launch family.svg thumb right 400px alt The NLS launch family would have shared a common liquid fuel engine. Proposed NLS family of launch vehicles. The National LaunchSystem or New LaunchSystem ... Program cancellation File Nationallaunchsystem.jpg thumb left A National LaunchSystem engine being ... program, the National LaunchSystem. Legacy Soon after the faster, better, cheaper Evolved Expendable Launch Vehicle EELV was proposed by the United States Air Force in 1994, Rocketdyne realized that they would ... of the National LaunchSystem ideal, albeit on a smaller scale. See also Human Explorations Framework Team 2010 2011 Space LaunchSystem 2010 Review of United States Human Space Flight Plans Committee ... Study 2005 Vision for Space Exploration 2004 Space Launch Initiative ca. 2002 2004 National Space Policy 1996 Space Launch Modernization Plan 1994 Spacelifter program 1993 Access to Space Study 1993 Advanced Transportation System Studies 1992 1994 National LaunchSystem 1991 1993 National aerospace ... Program Augustine Committee, 1990 Space Exploration Initiative 1989 Advanced LaunchSystem 1987 1990 List of space launchsystem designs Notes Reflist References citation author Boeing date ca. 2005 contribution Delta IV Heavy growth options for space exploration work Delta Launch 310 Delta IV Heavy ... LaunchSystem NLS url http www.fas.org spp military program launch nls.htm accessdate 2010 04 25 ... T. year 1992 title National launchsystem and its potential application to the launch of geosynchronous .... sfn Flight International 1991 p 12 A series of launch vehicles was proposed, based around the Space ... history from 1998 offers that reusable Single stage to orbit SSTO rockets and space planes such as the DC ... 2010 04 25 citation last Bush first George H. W. year 1991 title National Space Launch Strategy ... http www.fas.org spp military program launch eelv b.htm EELV Boeing Contains good summary of NLS from ... term NLS Category Shuttle derived space launch vehicles Category Cancelled space launch vehicles ... more details
Infobox rocket name Space LaunchSystem image Art of SLS launch.jpg imsize 300 Size of image omit px ... stage2thrust stage2SI stage2time stage2fuel The Space LaunchSystem , or SLS , is a Shuttle Derived ... LaunchSystem SLS reference configuration from February 2011 The Space LaunchSystem is a planned a heavy launch vehicle, derived from the Space Shuttle launchsystem. Its initial capability of the core ... LaunchSystem Booster last Morring first Frank publisher Aviation Week date 2006 6 16 accessdate June 20, 2011 ref On September 14, 2011, NASA announced its design selection for the new launchsystem ... accessdate September 14, 2011 ref ref name NASA Briefing on Deep Space LaunchSystem cite web url http ...?id 1567 title NASA s New Space LaunchSystem Announced publisher Space Ref . ref The initial two ... url http www.space.com 12957 nasa giant rocket space launchsystem infographic.html title Space Launch ... House of Representatives Hearing title A Review of the NASA s Space LaunchSystem work The Planetary ... rick tumlinson the senate launchsystem b 963484.html title The Senate LaunchSystem Destiny ... launchsystem disgraceful pork title Newt Gingrich Calls Space LaunchSystem Disgraceful Pork publisher ... issues the senate launchsystem title The Senate LaunchSystem publisher Competitive space ... use of space . ref cite web url http www.competitivespace.org issues the senate launchsystem title The Senate LaunchSystem publisher Competitive Space date September 15, 2011 ref Space Frontier Foundation ... links http www.nasa.gov exploration new space enterprise sls mpcv index.html Space LaunchSystem & Multi ... Preliminary Report on Multi Purpose Crew Vehicle and Space LaunchSystem PDF . NASA http www.youtube.com ... Reusablelaunch systems Spaceflight Category Partially reusable space launch vehicles Category NASA ... LaunchSystem cs Space LaunchSystem de Space LaunchSystem es Transbordador SLS fr Space LaunchSystem hr Space LaunchSystem it Space LaunchSystem he SLS nl Space LaunchSystem pl Space LaunchSystem ... more details
The Nanosatellite LaunchSystem NLS is a series of satellite launch missions coordinated by the Space Flight Laboratory of the University of Toronto Institute for Aerospace Studies . It provides a low cost launch service for nanosatellite s. ref cite web url http www.utias sfl.net SpecialProjects LaunchIndex.html title UTIAS SFL Low Cost Launch Program publisher University of Toronto Institute for Aerospace Studies, Space Flight Laboratory ref NLS 1 Launch date 30 June 2003 Launch vehicle Rockot Launch site Plesetsk Cosmodrome Participants flagicon Canada Canadian Advanced Nanospace eXperiment Program CanX 1 CanX 1 , flagicon Denmark AAUSAT 1, flagicon Denmark DTUsat NLS 2 Launch date 30 June 2003 Launch vehicle Rockot Launch site Plesetsk Cosmodrome Participants flagicon USA QuakeSat NLS 3 Launch date 27 October 2005 Launch vehicle Cosmos 3M Parent Spacecraft SSETI Express Launch site Plesetsk ... NLS 4 Launch date 28 April 2008 ref cite web url http www.utias sfl.net NLS 4 title Nanosatellite Launch ... ref Launch vehicle Polar Satellite Launch Vehicle PSLV C9 Launch site Satish Dhawan Space Centre , Second Launch Pad Participants flagicon Canada Canadian Advanced Nanospace eXperiment Program CanX ... 5 Launch date 28 April 2008 ref cite web url http www.utias sfl.net NLS 4 title Nanosatellite Launch ... ref Launch vehicle Polar Satellite Launch Vehicle PSLV C9 Launch site Satish Dhawan Space Centre , Second Launch Pad Participants flagicon Canada CanX 6 NTS NLS 6 Launch date July 12, 2010 ref cite news ... tracking spacecraft publisher BBC date 12 July 2010 ref Launch vehicle Polar Satellite Launch Vehicle PSLV C15 ref cite web url http www.utias sfl.net NLS 6 title Nanosatellite Launch Service 6 publisher University of Toronto Institute for Aerospace Studies, Space Flight Laboratory ref Launch site Satish Dhawan Space Centre , First Launch Pad Participants flagicon Norway AISSat 1, flagicon Switzerland ... Category Space launch vehicles space stub ... more details
Launch Abort System MLAS is a proposed alternative to the Max Faget invented tractor Launch Escape System LES currently planned for use by NASA for its Orion Constellation program Orion spacecraft in the event an Ares I malfunction during launch requires an immediate abort. A pad abort flight test ...&EDATE NASA Tests Alternate Launch Abort System for Astronaut Escape ref A primary test goal was the successful separation of a mock crew capsule from the abort system. Designed by NASA engineers and reported ... the theoretical reliability of the launch abort system by introducing more failure modes. Like ..., and the switch of the launch vehicle from Ares I with its perennial underperformance to Delta IV Heavy or SLS. July 2009 test launch A Max Launch Abort System test vehicle was launched July 8, 2009 ... the Orion spacecraft from aerodynamic stresses during launch, and to provide an interface between the spacecraft ..., which bolts atop of the Low Impact Docking System LIDS docking ring assembly. Second, the necessity ... ref The test vehicle was different from the actual system in many ways. The main difference is that the four .... The propulsion thrust was not balanced between the rockets by a manifold system, contrary to what is foreseen with the actual system. See also Boilerplate spaceflight Boilerplate commonscat inline Max Launch Abort System References refbegin http www.nasaspaceflight.com NASA Spaceflight main page http www.nasaspaceflight.com content ?cid 5300 NASA Spaceflight MLAS the alternative Orion Launch Abort System gains momentum full article http www.nasa.gov centers wallops missions mlas.html NASA page ... of successful pad abort test with launch photo accessed 8 July 2009 refend reflist Category Human ... more details
The United States Airborne Launch Control System ALCS is a method of assured command and control military ... Personnel The Airborne Launch Control System Flight of the 625th Strategic Operations Squadron provides ... Airborne Launch Control System Gallery File EC 135 1.png File EC 135 2.png File EC 135 3.png File ... 135 aircraft mission Emergency Rocket Communications System used shared UHF equipment at Launch facility ... ICBMs , the ALCS has the unique capability to retarget and launch the missiles without the interaction ... broadcasts to pass along information . This concept would allow communication to missile launch ... communication methods such as Emergency Rocket Communications System ERCS was giving the airborne crews the same degree of access to the launch facilities as the Launch control center ICBM underground ... s USAF Ballistic Missile Programs 1967 1968 , September 1969, pg 17 ref Minuteman launch facilities ... from the ALCS the destruction of the Launch control center ICBM launch control center or the hardenend intersite cable system would not prevent retaliation. ref http www.gwu.edu nsarchiv nukevault ebb249 ... Designation System Location Note 3 Mar 1967 BUSY LOBBY LGM 30 Minuteman Minuteman Vandenberg AFB , LF 5 First ALCS assisted launch 17 Apr 1967 BUSY MISSILE LGM 30 Minuteman Minuteman Vandenberg AFB , Vandenberg AFB Launch Facility 08 LF 08 28 Apr 1967 BUSY MUMMY LGM 30 Minuteman Minuteman Vandenberg AFB , Vandenberg AFB Launch Facility 02 LF 02 11 May 1967 BUSY FELLOW LGM 30 Minuteman Minuteman Vandenberg AFB , Vandenberg AFB Launch Facility 21 LF 21 25 Jan 1968 OLY TRIALS 7 LGM 30 Minuteman Minuteman II Vandenberg AFB , Vandenberg AFB Launch Facility 22 LF 22 12 Mar 1969 GIANT FIST 3 LGM 30 Minuteman Minuteman II Vandenberg AFB , Vandenberg AFB Launch Facility 04 LF 04 18 Apr 1969 SST M 3 LGM 30 Minuteman Minuteman II Vandenberg AFB , Vandenberg AFB Launch Facility 25 LF 25 18 Jun 1969 GLORY TRIP 37B LGM 30 Minuteman Minuteman II Vandenberg AFB , Vandenberg AFB Launch Facility 07 LF 07 ... more details
. Other advantages includes lower system weight, cost, and maintenance the ability to launch heavier ... carriers. In June 2010, the land based prototype of the system passed initial tests, with the first aircraft launch from the system taking place at the end of 2010. ref name aw emals cite web url ... 2010 p42 228803.xml date 7 June 2010 title Carrier LaunchSystem Passes Initial Tests publisher Aviation ... LaunchSystem EMALS url http www.navair.navy.mil lakehurst nlweb ieeerevc.pdf format PDF date 1994 ... during a test of the Electromagnetic Aircraft LaunchSystem EMALS at Naval Air Sys.jpg thumb The Electromagnetic Aircraft LaunchSystem at Naval Air Systems Command, Lakehurst, launching a United States ... 28, 2011 accessdate 2011 10 04 ref ref cite web title New carrier launchsystem tested url http www.upi.com Business News Security Industry 2011 10 03 New carrier launchsystem tested UPI 13601317652464 ... 228803.xml AVIATIONWEEK.COM Carrier LaunchSystem Passes Initial Tests ref Converteam UK is working ... www.janes.com news defence jni jni100726 1 n.shtml Converteam develops catapult launchsystem for UK ... driver References Reflist External links Commons category Electromagnetic Aircraft LaunchSystem http www.globalsecurity.org military systems ship systems emals.htm Electromagnetic Aircraft LaunchSystem ... Aircraft carriers Category Electromagnetic components da Electromagnetic Aircraft LaunchSystem ... in the EMALS. End Speed 28 103 m s Max Peak to Mean Tow Force Ratio 1.05 Launch Energy 122 MJ Cycle Time 45 seconds System Weight 225,000 kg System Volume 425 m Endspeed Variation 0 to 1.5 m s The Electromagnetic Aircraft LaunchSystem , commonly EMALS is a system under development by the United States Navy to launch carrier based aircraft from aircraft catapult catapults using a linear ... currents to generate magnetic fields that propel a carriage down a track to launch the aircraft ... within 45 seconds of a launch, faster than steam catapults. ref name howitworks Power conversion ... more details
The Improved Launch Control System ILCS was a system used by the United States Air Force s LGM 30 Minuteman Minuteman II ICBM force. ILCS was a method to transfer targeting information from a Minuteman Launch control center ICBM Launch Control Center to an individual missile by communications lines. Prior to ILCS, new missile guidance would have to be physically loaded at the Launch facility ICBM launch facility the process usually took hours. History ILCS was operational at most Minuteman II wings by . Minuteman III wings had a similar install, designated Command Data Buffer , providing the newer system the potential for remote retarging. ref Department of the Air Force Strategic Air Command Weapon Systems Acquisition 1964 1979 , 28 April 1980 ref Phaseout ILCS was phased out in mid 1990s by the retirement of the Minuteman II force, and the deactivation or reapportioning of units to Minuteman III. ref http www.fas.org nuke guide usa c3i react.htm FAS.org Rapid Execution and Combat Targeting ref Chronology 1979 1 Mar 341st Missile Wing 341 SMW s 490th Strategic Missile Squadron completes ILCS upgrades, at a cost of 365 million dollars ref http www.globalsecurity.org wmd agency 490ms.htm Globalsecurity.org 490th Missile Squadron ref See also Portal United States Air Force LGM 30 Minuteman Launch control center ICBM Command Data Buffer Minuteman III upgrade similar to ILCS Rapid Execution and Combat Targeting System REACT References Reflist Category Nuclear command and control Category Cold War weapons of the United States Category Nuclear weapons of the United States USAF stub ... more details
crew module. Image Launch escape system diagram.jpg thumb Apollo spacecraft Apollo Launch Escape System. A Launch Escape System LES is a top mounted rocket connected to the crew module of a crewed ... which later became the Lockheed Propulsion Company . Apollo used Apollo spacecraft Launch Escape System .28LES.29 a design that had many similarities to the Mercury system. Launch Escape Systems ... spacecraft uses a liquid fueled launch abort system integrated to the capsule to minimize spacecraft costs. The LES may be used while the launch vehicle is still on the launch pad , or during ... the shuttle program will use a Mercury and Apollo style escape rocket system, while an alternative system, called the Max Launch Abort System MLAS , ref http www.nasaspaceflight.com content ?cid ... news n1002 18orionlas title Orbital sees bright future for Orion launch abort system author Stephen ... 1 Launch Escape System LES abort test from launch pad with Apollo Boilerplate spaceflight Boilerplate ...?media id 13781635 NASA Pad Abort 1 Flight Test Video Highlights DEFAULTSORT Launch Escape System ... it Launch Escape System hu Ment rak ta ja pl Rakietowy System Ratunkowy LES pt Sistema ... from the launch pad to a height sufficient for its parachutes to open. Consequently, they must make ... into the bullet shaped protective launch shroud. Under NASA s Commercial Crew Development CCDev program ... the attempt to launch Soyuz T 10 1 on September 26, 1983. The rocket caught fire, just before launch ... mi from the launch pad. On the Soyuz, the grid fin s also deploy on the payload fairing to stabilize the craft. File 10073418.jpg thumb The escape system unintentionally blasted off from the Mercury spacecraft on the failed Mercury Redstone 1 mission A previous launch accident occurred during ... Boilerplate B 23A. References Reflist External links commonscat Launch escape systems http www.apollosaturn.com asnr escape.htm Launch Escape Subsystem Detailed description of the Apollo launch escape ... more details
The Launch Processing System LPS is an automated, computer controlled system at the Kennedy Space Center KSC which oversees and coordinates the processing and checkout of systems and components for the Space Shuttle launch vehicle and its payloads. ref name LPS1 cite web url http science.ksc.nasa.gov facilities lps.html title KSC s Automated Launch Processing System publisher NASA accessdate July 20, 2009 ref The LPS automatically performs tests on much of the vehicle components as they are being readied for launch, and alerts operators if any anomalies are detected. ref name LPS2 cite web url http science.ksc.nasa.gov shuttle technology sts newsref sts lcc.html title Launch Control Center publisher NASA accessdate July 20, 2009 ref The LPS also manages the launch countdown events, culminating in a successful launch. Function Early in the design of the Space Shuttle program, the expected launch rate was 12 flights per year. ref name COF1 cite web url http www.century of flight.net Aviation 20history space Space 20Shuttle 20history.htm title Space Shuttle History publisher Century of Flight accessdate July 20, 2009 ref The LPS was designed to oversee and manage the parallel processing of multiple orbiters and their subsystems in order to meet this launch schedule. ref name LPS1 The LPS tracks and manages all components of the Space Shuttle launch vehicle from the time the individual components arrive at KSC, through checkout, integration, testing, installation, and finally culminating in a launch. Any time a component is functioning, sensors within the component relay data on its ... program launch. ref name LPS1 Components The LPS is composed of 3 major subsystems the Checkout ... Subsystem CCMS controls the actual processing and launch of the Space Shuttle. ref name LPS3 This subsystem ... transmission and recording systems, which monitor the pre launch performance of all electrical and mechanical ... Center SDC ref name LPS1 The CDS SDC is located on the second floor of the Launch Control Center . Record ... more details
Cleanup date May 2009 Infobox Spacecraft Name HL 20 Personnel LaunchSystem Image File HL20 mockup.jpeg ... Refs The HL 20 Personnel LaunchSystem was a circa 1990 NASA spaceplane concept for manned ... to as a Personnel LaunchSystem PLS , could utilize the HL 20 and an expendable launchsystem ... launch site. ref name Nsum http www.nasa.gov centers langley news factsheets HL 20.html NASA.gov HL 20 model for Personnel LaunchSystem research ref full Proposed missions Image EL 1996 00177.jpeg ... to several launch vehicle concepts. Titan III was an existing booster system which could have been used ... launchsystem option would have been the National LaunchSystem under study by the Air Force and NASA in the 90 s. Choice of a launchsystem for the HL 20 PLS would depend both on the required date ... 20.html NASA.gov HL 20 model for Personnel LaunchSystem research http www.youtube.com watch?v J5i2DS9bzkM HL 20 Personnel LaunchSystem video http www.youtube.com watch?v lZ 66UcAmKk&feature related ... 20 20MODEL.pdf Improving the Subsonic Performance of Proposed Personnel LaunchSystem Concept http ... Full Scale Research Model DEFAULTSORT Hl 20 Personnel LaunchSystem Category Lifting body aircraft ... Earth orbit, i.e., a small space taxi system. Although never approved for development, the PLS concept ... to the manned launch capability of the United States for three main reasons ref name Nsum Assured ... recover the crew during critical phases of the launch and return from orbit. Affordable costs. As a small ... s approach uses a blunt cone shape with a parachute landing system, clarify date December 2010 ... following launch on a Saturn IB . The HL 20 PLS concept has evolved from these early shapes and based ... horizontally in a vehicle processing facility while an expendable launch vehicle is processed vertically in a separate facility. The launch vehicle and HL 20 would be mated at the launch pad and the launch sequence initiated as the space station passes over the launch site. Following launch, the HL ... more details
orbit br TLI Trans Lunar Injection br List of space launchsystem designs covers ref name lindroos citation url http www.pmview.com spaceodysseytwo spacelvs index.htm title Introduction To Future Launch ..., and or proposals for launch systems such as rockets and reusable spaceplane s, typically for orbit ing the Earth . Plans may mature into an actual launchsystem, or may not be developed. An example of launch vehicle plan, is the Space LaunchSystem proposed by NASA in 2011, which is planning ... Lift Launch Vehicle 2010 Shuttle Derived Heavy Lift Launch Vehicle Side mount , a non reusable, cargo oriented Space Shuttle Shuttle based launch vehicle with payload capacity 100 35 75 tons for the heaviest ... LaunchSystem 2011 ref cite web url http www.aviationweek.com aw generic story channel.jsp?channel ... 20Launch 20System 20Boosters title NASA Will Compete Space LaunchSystem Booster last Morring first Frank publisher Aviation Week date accessdate June 20, 2011 ref A NASA Space Shuttle based launchsystem ... 192,900 lb to LEO. ref name shuttlez U.S. National LaunchSystem designs 1991 Studied in the year ... web url http www.fas.org spp military program launch nls.htm title National New LaunchSystem publisher ... Lockheed Reusable Orbital Carrier 1963 ref name lindroos Lockheed System III & IV 1963 ref name ... name lindroos NASA Shuttle II Advanced Manned LaunchSystem studies 1978 89 ref name lindroos Spacejet ... LaunchSystem 1989 ref name lindroos Boeing United States Air Force USAF Air Launched Sorite Vehicle ... Programme 2004 Space Launch Initiative designs 2000 ref cite web url http www.nasa.gov centers marshall news background facts slifactstext02.html publisher NASA title Space Launch Initiative fact sheet ... 20080043657 2008043384.pdf title A Near Term, High Confidence Heavy Lift Launch Vehicle format PDF date accessdate 2011 09 29 ref . The vehicle is also known as Shuttle Derived Heavy Lift Launch Vehicle, High Confidence Heavy Lift Launch Vehicle, and HLV. In a picture shown at the 17 June ... more details
Multiple issues unreferenced May 2008 notability May 2008 confusing May 2008 The Integrated Launch and Recovery Television Surveillance System ILARTS provides the Landing Signal Officer with a reference for aircraft lineup and glideslope information during recovery operations aboard US aircraft carrier s, and is used as a debriefing medium for pilots. Additionally, the system is used for recording significant flight deck events and, when necessary, for mishap or incident analysis. Category Aircraft carriers aviation stub ... more details
Infobox Weapon is missile yes name Non Line of Sight LaunchSystem image Image nlosls1.jpg 300 px caption ... Martin and Raytheon production date Canceled type Self contained missile launchsystem speed weight convert 3150 lb ST LT lk out abbr on launch platform CLU of 15 canistered missiles on truck, ship ... on unit cost US 466,000 per missile The Non Line of Sight LaunchSystem NLOS LS was a self contained missile launcher system that was under development by NETFIRES LLC, a partnership between Lockheed Martin and Raytheon . Each Container Launch Unit CLU holds 15 missiles, and a self locating networked communications system. CLUs can be linked for coordinated launching, with the missiles fired and controlled remotely via autonomous vertical launch. The weapon is roughly 2 meters tall. The program ... Non Line of Sight LaunchSystem Lockheed Martin http www.designation systems.net dusrm app4 ... net fires.htm Non Line of Sight LaunchSystem NLOS LS Global Security http www.defense update.com ... Non Line of Sight LaunchSystem mr ja NLOS LS ru NLOS LS ... on Length convert 60 in mm abbr on Guidance GPS Inertial guidance system INS , Infrared homing imaging ... guidance system INS , laser radar LADAR seeker with automatic target recognition . ref name DESSYS ... ref April 2007 Successful test launch of a Precision Attack Missile from a CLU at White Sands Missile ...?guid 7B71201188 8991 4CD4 8499 B7B533BC53AC 7D NetFires LLC Precision Attack Missile Launch Paves the Way for Complete System Testing Netfires LLC PR ref June 2007 Successful test of Precision Attack ... fired from Container Launch Unit. Scores hit on T 72 tank. ref cite web url http www.spacewar.com reports NLOS LS Team Completes First Test Of Missile Fired From Container Launch Unit 999.html title NLOS LS Team Completes First Test Of Missile Fired From Container Launch Unit publisher Spacewar.com ... date 2010 04 23 accessdate 2011 05 27 ref 3 May 2010 The U.S. Army removes the system from their website ... more details
Infobox Weapon name M270 Multiple Launch Rocket System MLRS image Image MLRS 05.jpg 300px caption M270 ... Launch Rocket System M270 MLRS is an armored , self propelled artillery self propelled , multiple ... thumb right The M270 MLRS conducts a rocket launch. Image MLRS system.JPEG thumb right MLRS System with launch vehicle, loader and a command center inside an APC When first deployed with the U.S. Army ... www.army technology.com projects mlrs specs.html Army Technology MLRS Multiple Launch Rocket System ... numbers References reflist External links Commons Multiple Launch Rocket System http www.army technology.com ... System ja MLRS no M270 MLRS pl M270 MLRS ru M270 Multiple Launch Rocket System fi M270 MLRS sv M270 ... ballistic missiles, such as the U.S. Army Tactical Missile System ATACMS , it can hit targets convert ..., Germany, and France. It was developed from the older General Support Rocket System GSRS . The M270 MLRS weapons system is collectively known as the M270 MLRS Self propelled Loader Launcher SPLL . The SPLL ... the electronic Fire Control System, is mated to the M993 Carrier Vehicle. The M993 is a derivative ... winch system. All twelve rockets or two ATACMS missiles can be fired in under a minute. One ... helicopters ready for action , Daily Telegraph , April 21, 1999. ref Metric system metric maps ... updated , Defense Industry Daily, August 2, 2006. ref A German developmental artillery system, called ... shells. The M270 system can fire MFOM, MLRS Family Of Munition rockets and artillery missiles .... M27 United States Completely inert training Launch Pod Container to allow full loading cycle ... 2010 ref M39 United States Army Tactical Missile System Army TACMS , with a range of 97 km with 950 ... warhead VX nerve agent . Not standardized. MGM 140A United States Army Tactical Missile System ... system INS M30 404 M85 DPICM submunitions br M31 90 kg 200 lb unitary HE AT2 SCATMIN 254 ... 227mm Multiple Launched Rocket System MLRS ref Height max elevation not available Max road speed ... more details
wiktionarypar launchLaunch may refer to In boating Launch boat , a large motor boat Motor Launch ML , a small military vessel used by the Royal Navy Ship naming and launching , when a ship or boat is dispatched from a slipway, prior to fitting out and commissioning In other uses Launch Dragon Ball Launch Dragon Ball , a character in Dragon Ball media Rocket launch , first phase of a rocket flight Air launch , the practice of dropping an aircraft, rocket, or missile from a mothership LAUNCH Media , creators of LAUNCH magazine and LAUNCH.com LAUNCHcast , an Internet radio service offered by Yahoo Music Sea Launch , ocean based space launch company See also Lunch or luncheon disambig es Lanzamiento ... more details
Infobox Single Name The Launch Cover DJ Jean The Launch.jpg Caption United Kingdom cover art Artist DJ Jean from Album Released February 2, 1999 small Netherlands small br August 30, 1999 small UK small Format CD single , CD maxi , 12 12 maxi B side Remix Genre Euro house Length 6 46 small original small 3 38 small radio edit small Label Mo Bizz Recordings Writer Koen Groeneveld br Addy van der Zwan br Jan Voermans br Jan Engelaar Producer Klubbheads br DJ Jean Last single U Got My Love br 1998 This single The Launch br 1999 Next single Love Come Home br 2000 Extra musicsample filename DJ Jean The Launch.ogg format Ogg title The Launch 1999 Type single The Launch is the title of a Euro house song produced by Dutch people Dutch disc jockey , DJ Jean and Klubbheads . The vocals are performed by Natasja Morales. It was released in the Netherlands on February 2, 1999 and released in the United Kingdom on August 30, 1999. The song was considered a big hit in Europe , it was number one on the Netherlands pop charts and was number two in the United Kingdom . The song receives constant airplay at many hockey games in Canada and the United States . Track listings CD single Netherlands ref http www.discogs.com DJ Jean The Launch release 28083 The Launch release info ref The Launch Radio Edit The Launch Rollercoaster s Pumped Up Mix The Launch Original Mix The Launch Instant Double Remix Peak positions class wikitable sortable Chart 1999 align center Peak br position Ultratop 50 Belgian Flanders Singles Chart align center 14 RPM magazine Canadian RPM Dance Chart align center 4 Dutch Top 40 align center 1 Eurochart Hot 100 Singles align center 11 SNEP French SNEP Singles Chart align center 28 German Singles Chart align center 92 Swedish Singles Chart align center 40 UK Singles Chart ... Time br by Britney Spears end box References Reflist DEFAULTSORT Launch Category 1999 singles Category Dutch Top 40 number one singles nl The launch ... more details
Infobox rocket image ISAS JAXA RVT Flight Test.jpg caption Reusable Vehicle Testing Reusable Vehicle Testing flight. name RVT function Technology demonstrator for liquid propulsion based VTOL rocket flight manufacturer Institute of Space and Astronautical Science ISAS JAXA country origin Japan The Reusable Vehicle Testing RVT project was conducted by the Japanese Space Agency JAXA from 1998 until 2003. The project involved a series of experimental vehicles to test repeated flights of a reusable rocket. Four complete vehicles were developed during the project. The design of the experimental vehicles addressed various technical challenges for future ReusablelaunchsystemReusableLaunch Vehicles RLV such as flight on demand, quick turnaround, higher performance, lightweight structures and materials. The project involved ground and flights tests with the flight testing conducted at the Institute of Space and Astronautical Science Institute of Space and Astronautical Science ISAS Noshiro Testing ... control system mounted at the top of the airframe. The frame around the bottom of the tanks ... guidance and control system. March 13 to March 26, 1999 RVT 3 During the experiments of period ... reusable rocket, demonstrating a number technologies. Engine pressurization was by a gas ... of 70 over the promotion of high thrust zone, to assess the suitability of the system to obtain ... a reusable high altitude rocket based on the technologies demonstrated in the RVT project. http ...?itemid 3966 RVT derived reusable sounding rocket proposal at Hobbyspace http www.spacefuture.com archive flight demonstration and a concept for readiness of fully reusable rocket vehicles.shtml Technical paper Flight Demonstration and a Concept for Readiness of Fully Reusable Rocket Vehicles ... to the Reusable Sounding Rocket , Norway Japan Symposium on Polar, Space, and Climate Research May 29. 2007 Category Japanese space program Category Reuse fr Reusable Vehicle Testing ja ... more details
Context date October 2009 Reusable Asset Specification is an Object Management Group standard to package digital artifacts. The specification is a set of guidelines and recommendations about the structure, content, and descriptions of reusable software assets. The main purpose of RAS is to increase the reusability of the software assets by encouraging consistent and standard packaging. External links http www.omg.org technology documents formal ras.htm OMG Reusable Asset Specification page Category Standards standard stub ... more details
Multiple issues cleanup February 2009 introrewrite February 2009 refimprove December 2009 File Blue reusable shopping bag.JPG thumb A blue reusable shopping bag A reusable shopping bag , sometimes called ..., or a thick plastic that is more durable than disposable plastic bags, allowing multiple use. Reusable ... shops. Reusable shopping bags require more energy to produce than common plastic shopping bags. One reusable bag requires the same amount of energy as an estimated 28 traditional plastic shopping ... plastic bag, a canvas or cotton reusable bag would have to be reused a total of 171 times ... increasingly discourage consumers from using disposable plastic bags and offer alternative reusable ... a dialectical perspective ref Because of these encouragements, reusable shopping bags are gradually taking place beside plastic bags. The shape of reusable shopping bags which are now becoming popular ... industry promotes reusable shopping bags as sustainable fashion . Many supermarket s encourage the use of reusable shopping bags to increase sales and profit margins. Most non woven polypropylene bags ... for bringing in reusable bags. ref name cash discount cite news url http www.usatoday.com money industries ... url http www.whiteapricot.com fab finds rm reusable shopping bags.php title Eco friendly Reusable Shopping ... reusable bags were imported into the United States for resale and give aways under Harmonized Tariff ... with the rise of environmental claims of reusable bag reseller in the United States from 130 ... bags has provided a natural alternative to single use plastic bags and reusable plastic bags. Over 25 million have been sold in the UK. Reusable plastic bags do not have a simple end of life disposal ... friendliness and usual though far from universal green color. Green Bags and similar reusable ... volume of reusable bags being imported and resold, along with the 2008 Wall Street Journal article ... retail carrier bags 10 of total as reported by the Wall Street Journal which translated to each reusable ... more details
to the launch pad. ref cite web url http www pao.ksc.nasa.gov kscpao release 1985 252 85r.htm title LAUNCH COMPLEX 39, PADS A AND B publisher NASA KSC year 1992 ref A similar system is used to launch ... Image Stspad39baerial.jpg thumb right 300px Kennedy Space Center Launch Complex 39 A launch pad is the area and facilities where rockets or spacecraft lift off. A spaceport or rocket launch site can contain one or many launch pads. A typical launch pad consists of the service and umbilical structures. The service structure provides an access platform to inspect the launch vehicle prior to launch ... propellent loading, gas, power, and communication links to the launch vehicle. The launch vehicle sits atop of the launch platform, which has the flame deflection structure to withstand the intense heat and load generated by rocket engines during liftoff. Most cryogenic launch vehicles need to be continuously .... Without the ability to top off the launch vehicle, the launch would have to be scrubbed ... on launch pads to meet these types of servicing requirements both during launch and in the preparation ... met by the use of explosive bolt s to connect the launch vehicle to the pad. When the vehicle is stable and ready to fly the bolts explode, severing the vehicle s ties to the launch pad and structures on the ground. Transport of rockets to the pad There are several different types of launch site, determined ... 2 , travelled horizontally with its tail forward to the launch site at Peenem nde . This is the most ... Buran . In a similar manner, at the Soviet launch site near Volgograd , a silo used to launch test ... visible above ground. Hence no surface pad is used Russian silos are reusable. This method ... IB rockets launched from Launch Complex 39 at the Kennedy Space Center in the past, the Space Shuttle ... the Titan launch vehicle and its mobile launcher platform from the integration building to the launch ... at Kennedy Space Center Launch Complex 39 for the Saturn V. It was rejected for that application ... more details
Encyclopedia
top
