[{"@context":"http:\/\/schema.org\/","@type":"BlogPosting","@id":"https:\/\/wiki.edu.vn\/en\/wiki8\/hypersonic-flight-experiment-wikipedia\/#BlogPosting","mainEntityOfPage":"https:\/\/wiki.edu.vn\/en\/wiki8\/hypersonic-flight-experiment-wikipedia\/","headline":"Hypersonic Flight Experiment – Wikipedia","name":"Hypersonic Flight Experiment – Wikipedia","description":"before-content-x4 From Wikipedia, the free encyclopedia For Japan’s reentry demonstrator prototype called “Hypersonic Flight Experiment”, see HYFLEX. after-content-x4 Reusable Launch","datePublished":"2019-06-15","dateModified":"2019-06-15","author":{"@type":"Person","@id":"https:\/\/wiki.edu.vn\/en\/wiki8\/author\/lordneo\/#Person","name":"lordneo","url":"https:\/\/wiki.edu.vn\/en\/wiki8\/author\/lordneo\/","image":{"@type":"ImageObject","@id":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","url":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","height":96,"width":96}},"publisher":{"@type":"Organization","name":"Enzyklop\u00e4die","logo":{"@type":"ImageObject","@id":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","url":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","width":600,"height":60}},"image":{"@type":"ImageObject","@id":"https:\/\/upload.wikimedia.org\/wikipedia\/commons\/thumb\/6\/62\/RLV-TD_HEX01%2C_TDV_being_transported.jpg\/220px-RLV-TD_HEX01%2C_TDV_being_transported.jpg","url":"https:\/\/upload.wikimedia.org\/wikipedia\/commons\/thumb\/6\/62\/RLV-TD_HEX01%2C_TDV_being_transported.jpg\/220px-RLV-TD_HEX01%2C_TDV_being_transported.jpg","height":"147","width":"220"},"url":"https:\/\/wiki.edu.vn\/en\/wiki8\/hypersonic-flight-experiment-wikipedia\/","wordCount":3156,"articleBody":"     (adsbygoogle = window.adsbygoogle || []).push({});before-content-x4From Wikipedia, the free encyclopediaFor Japan’s reentry demonstrator prototype called “Hypersonic Flight Experiment”, see HYFLEX.       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4Reusable Launch Vehicle Hypersonic Flight Experiment or RLV HEX was the first test flight in the RLV Technology Demonstration Programme of the Indian Space Research Organisation (ISRO). The demonstration trials will pave the way for a two-stage-to-orbit (TSTO) fully re-usable launch vehicle. HEX was launched on 23 May 2016.[2][3][4]       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4Table of ContentsConfiguration[edit]Thermal Protection System[edit]Objectives[edit]Mission profile[edit]See also[edit]References[edit]Configuration[edit]First stage: live, 9 ton solid booster (S-9)Second stage: winged test vehicle, no main engines (scramjet will be used in the future)In 2009, an airframe engineering model, axisymmetric proto nose cap after graphitisation (C-C) and slow burn rate propellant were completed. Aerodynamic characterization of technology demonstration vehicle was completed at National Aerospace Laboratories (NAL), Vikram Sarabhai Space Centre (VSSC) and Indian Institute of Space Science and Technology (IIST). Computational flow simulation and supersonic combustion in ground testing were also completed.RLV-TD consists of a fuselage (body), a nose cap, double delta wings and twin vertical rudders. It has active control surfaces called Elevons and Rudders.[4] Apart from the twin rudders it is similar in shape and operation to a small Space Shuttle Orbiter.Thermal Protection System[edit]  TDV uses 600 or so heat resistant silica tiles and Flexible External Insulation, nose-cap is made out Carbon-Carbon composite with SiC coating. The leading edges of twin rudders are Inconel-718, wing leading edges of 15CDV6.[5][6][7][8][9][10]       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4Objectives[edit]HEX was the first test flight of a reusable launch vehicle developed by India. The test flight objectives included:[11]Validating the aerodynamic design characteristics during hypersonic flightCharacterize induced loads during the hypersonic descent through the atmosphereAssess the performance of the carbon fibre used in construction of the nose of the vehicleDemonstrate first stage separation sequencingMission profile[edit]The Hypersonic Flight Experiment, or HEX, was the first test-flight in the RLV Technology Demonstration Programme.  The RLV-TD vehicle was launched from the first launchpad of Satish Dhawan Space Centre on 23 May 2016 at 7:00 AM local time, on board an HS9 rocket booster.[12]After a successful lift that lasted 91.1 seconds to a height of about 56\u00a0km, the RLV-TD separated from the 9-ton HS9 booster and further ascended to a height of about 65\u00a0km. The RLV-TD then began its descent at about Mach 5 (five times the speed of sound). The vehicle’s navigation, guidance and control systems accurately steered the vehicle during this phase for a controlled splashdown down to the defined landing spot over the Bay of Bengal, at a distance of about 450\u00a0km from Sriharikota, thereby fulfilling its mission objectives.The vehicle was tracked during its flight from ground stations at Sriharikota and a shipborne terminal. The total flight duration from launch to splashdown lasted about 773.6 seconds.[13] The unit was not planned to be recovered.[14][15]  ISRO plans to construct an airstrip greater than 4\u00a0km long in Sriharikota island in the “near future”.[16]  Critical technologies such as autonomous navigation, guidance & control, reusable thermal protection system, and descent mission management were validated in this flight.See also[edit]References[edit]^ “RLV-TD HEX-01 mission accomplished successfully”. Indian Space Research Organisation. isro.gov.in. May 23, 2016. Retrieved May 23, 2016.^ ““India’s First-Ever Indigenous Space Shuttle RLV-TD Launched Successfully”“.^ India\u2019s Reusable Launch Vehicle-Technology Demonstrator (RLV-TD), Successfully Flight Tested Archived 2021-02-09 at the Wayback Machine. 23 May 2016. ISRO.^ a b RLV-TD Archived 2021-04-17 at the Wayback Machine. ISRO. 23 May 2016. Includes diagrams.^ Kumar, Kiran. ““Indigenous Development of Materials for Space Programme”“. Retrieved 30 June 2020.^ “SILICA TILES AS A THERMAL PROTECTION FOR RLV-TD” (PDF). Retrieved 30 June 2020.^ “Current Science Volume 114 – Issue 01”. Retrieved 30 June 2020.^ “The technology behind India’s Reusable Launch Vehicle”. Retrieved 30 June 2020.^ “A Deep Dive Into ISRO’s Reusable Launch Vehicle Technology \u2013 Part I”. Retrieved 30 June 2020.^ “A Deep Dive Into ISRO’s Reusable Launch Vehicle Technology \u2013 Part II”. Retrieved 30 June 2020.^ An Indian space shuttle takes shape 2009^ Bagla, Pallava (2 May 2016). “Swadeshi Space Shuttle Tests, ISRO’s ‘Mission Accomplished’: 10 Facts”. DDTV. India. Retrieved 2016-05-25.^ Yadav, Sandeep; Jayakumar, M.; Nizin, Aziya; Kesavabrahmaji, K.; Shyam Mohan, N. (2017-12-01). “Final Phase Flight Performance and Touchdown Time Assessment of TDV in RLV-TD HEX-01 Mission”. Journal of the Institution of Engineers (India): Series C. 98 (6): 679\u2013688. Bibcode:2017JIEIC..98..679Y. doi:10.1007\/s40032-017-0403-9. ISSN\u00a02250-0553. S2CID\u00a0115904439.^ “India’s Reusable Launch Vehicle Successfully Flight Tested”. ISRO website. Archived from the original on 14 September 2016. Retrieved 23 May 2016.^ “ISRO successfully launches Indias first ever indigenous space shuttle”. The Economic Times. Retrieved 24 May 2016.^ “ISRO Gears up for 6 Major Missions This Year”. Express News Service. 30 May 2015.     (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4"},{"@context":"http:\/\/schema.org\/","@type":"BreadcrumbList","itemListElement":[{"@type":"ListItem","position":1,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki8\/#breadcrumbitem","name":"Enzyklop\u00e4die"}},{"@type":"ListItem","position":2,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki8\/hypersonic-flight-experiment-wikipedia\/#breadcrumbitem","name":"Hypersonic Flight Experiment – Wikipedia"}}]}]