Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Max_Launch_Abort_System> ?p ?o }
Showing triples 1 to 71 of
71
with 100 triples per page.
- Max_Launch_Abort_System abstract "The Max 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 spacecraft in the event an Ares I malfunction during launch requires an immediate abort.A "pad abort" flight test of the MLAS was performed at NASA's Wallops Flight Facility on July 8, 2009 just after 6:25 a.m. A primary test goal was the successful separation of a mock crew capsule from the abort system.Designed by NASA engineers and reported on the website nasaspaceflight.com on December 6, 2007, the proposed MLAS uses 4 existing Thiokol-Huntsville built solid-rocket motors (built in 1988) placed at 90° intervals within the Orion's bullet-shaped protective cover (fairing). The protective cover was originally designed to protect the Orion spacecraft from aerodynamic stresses during launch, and to provide an interface between the spacecraft's crew module with the LES.The MLAS is designed with the aim of reducing the height of the Orion/Ares I stack while also reducing weight and center-of-gravity issues of a traditional LES. The bullet-shaped MLAS is also expected to provide better aerodynamic qualities during the first two minutes of flight, reducing stresses when the vehicle encounters the "Max Q" regions of hypersonic flight. The MLAS is also expected to simplify production, as existing hardware would be employed.There are several drawbacks to MLAS. First, the bullet-shaped protective cover would have to be modified and reinforced to allow for the use of the solid-rocket motors, something not needed with the LES, which bolts atop of the LIDS docking ring assembly. Second, the necessity to fire multiple motors (LES uses one motor and multiple nozzles) simultaneously for an abort decreases the theoretical reliability of the launch abort system by introducing more failure modes.Like the existing LES, the MLAS would provide protection to the Orion spacecraft crew during the first 2½ minutes of flight, with the MLAS being jettisoned, along with the service module's fairing panels, after the solid-rocket first stage is jettisoned. If implemented, the Orion/Ares I stack would resemble the towerless Gemini-Titan stack used between 1965–66, in which ejection seats were used as the primary form of escape for the astronauts who flew on the ten Gemini missions.The MLAS concept was dropped with the transformation of the Crew Exploration Vehicle into the Orion Multi-Purpose Crew Vehicle, and the switch of the launch vehicle from Ares I (with its perennial underperformance) to Delta IV-Heavy or SLS.".
- Max_Launch_Abort_System thumbnail MLAS_components.jpg?width=300.
- Max_Launch_Abort_System wikiPageExternalLink ESN.
- Max_Launch_Abort_System wikiPageExternalLink mlas.html.
- Max_Launch_Abort_System wikiPageExternalLink HQ_M09-110_MLAS_June_22.html.
- Max_Launch_Abort_System wikiPageExternalLink image_feature_1406.html.
- Max_Launch_Abort_System wikiPageExternalLink www.nasaspaceflight.com.
- Max_Launch_Abort_System wikiPageExternalLink ?cid=5300.
- Max_Launch_Abort_System wikiPageExternalLink viewsr.html?pid=31486.
- Max_Launch_Abort_System wikiPageID "14664973".
- Max_Launch_Abort_System wikiPageLength "5641".
- Max_Launch_Abort_System wikiPageOutDegree "23".
- Max_Launch_Abort_System wikiPageRevisionID "642752638".
- Max_Launch_Abort_System wikiPageWikiLink Ares_I.
- Max_Launch_Abort_System wikiPageWikiLink Boilerplate_(spaceflight).
- Max_Launch_Abort_System wikiPageWikiLink Category:Ares_(rocket_family).
- Max_Launch_Abort_System wikiPageWikiLink Category:Articles_containing_video_clips.
- Max_Launch_Abort_System wikiPageWikiLink Category:Human_spaceflight.
- Max_Launch_Abort_System wikiPageWikiLink Category:Spacecraft_components.
- Max_Launch_Abort_System wikiPageWikiLink Crew_Exploration_Vehicle.
- Max_Launch_Abort_System wikiPageWikiLink Ejection_seat.
- Max_Launch_Abort_System wikiPageWikiLink Ejection_seats.
- Max_Launch_Abort_System wikiPageWikiLink Gemini_spacecraft.
- Max_Launch_Abort_System wikiPageWikiLink Launch_Escape_System.
- Max_Launch_Abort_System wikiPageWikiLink Launch_escape_system.
- Max_Launch_Abort_System wikiPageWikiLink Low_Impact_Docking_System.
- Max_Launch_Abort_System wikiPageWikiLink Max_Faget.
- Max_Launch_Abort_System wikiPageWikiLink Max_Q.
- Max_Launch_Abort_System wikiPageWikiLink Maxime_Faget.
- Max_Launch_Abort_System wikiPageWikiLink NASA.
- Max_Launch_Abort_System wikiPageWikiLink NASA_Docking_System.
- Max_Launch_Abort_System wikiPageWikiLink Orion_(Constellation_program).
- Max_Launch_Abort_System wikiPageWikiLink Orion_(spacecraft).
- Max_Launch_Abort_System wikiPageWikiLink Orion_Multi-Purpose_Crew_Vehicle.
- Max_Launch_Abort_System wikiPageWikiLink Payload_fairing.
- Max_Launch_Abort_System wikiPageWikiLink Project_Gemini.
- Max_Launch_Abort_System wikiPageWikiLink Rocket_fairing.
- Max_Launch_Abort_System wikiPageWikiLink Titan_II_GLV.
- Max_Launch_Abort_System wikiPageWikiLink Wallops_Flight_Facility.
- Max_Launch_Abort_System wikiPageWikiLink File:Fabrication_and_launch_of_the_Max_Launch_Abort_System_-_July_8_-_2009.ogg.
- Max_Launch_Abort_System wikiPageWikiLink File:MLAS_components.jpg.
- Max_Launch_Abort_System wikiPageWikiLink File:MLAS_concept_of_operations.jpg.
- Max_Launch_Abort_System wikiPageWikiLinkText "Max Launch Abort System".
- Max_Launch_Abort_System hasPhotoCollection Max_Launch_Abort_System.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Commonscat-inline.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Convert.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Include-NASA.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Multiple_issues.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Project_Constellation.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Refbegin.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Refend.
- Max_Launch_Abort_System wikiPageUsesTemplate Template:Reflist.
- Max_Launch_Abort_System subject Category:Ares_(rocket_family).
- Max_Launch_Abort_System subject Category:Articles_containing_video_clips.
- Max_Launch_Abort_System subject Category:Human_spaceflight.
- Max_Launch_Abort_System subject Category:Spacecraft_components.
- Max_Launch_Abort_System hypernym Alternative.
- Max_Launch_Abort_System type Article.
- Max_Launch_Abort_System type Organisation.
- Max_Launch_Abort_System type Article.
- Max_Launch_Abort_System type Component.
- Max_Launch_Abort_System type Source.
- Max_Launch_Abort_System type Vehicle.
- Max_Launch_Abort_System comment "The Max 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 spacecraft in the event an Ares I malfunction during launch requires an immediate abort.A "pad abort" flight test of the MLAS was performed at NASA's Wallops Flight Facility on July 8, 2009 just after 6:25 a.m.".
- Max_Launch_Abort_System label "Max Launch Abort System".
- Max_Launch_Abort_System sameAs m.03gscqc.
- Max_Launch_Abort_System sameAs Q6794960.
- Max_Launch_Abort_System sameAs Q6794960.
- Max_Launch_Abort_System wasDerivedFrom Max_Launch_Abort_System?oldid=642752638.
- Max_Launch_Abort_System depiction MLAS_components.jpg.
- Max_Launch_Abort_System isPrimaryTopicOf Max_Launch_Abort_System.