Indian Space Research Organization
  • Home
  • Business
    • Internet
    • Market
    • Stock
  • Parent Category
    • Child Category 1
      • Sub Child Category 1
      • Sub Child Category 2
      • Sub Child Category 3
    • Child Category 2
    • Child Category 3
    • Child Category 4
  • Featured
  • Health
    • Childcare
    • Doctors
  • Home
  • Business
    • Internet
    • Market
    • Stock
  • Downloads
    • Dvd
    • Games
    • Software
      • Office
  • Parent Category
    • Child Category 1
      • Sub Child Category 1
      • Sub Child Category 2
      • Sub Child Category 3
    • Child Category 2
    • Child Category 3
    • Child Category 4
  • Featured
  • Health
    • Childcare
    • Doctors
  • Uncategorized

Friday, January 11, 2019

Reusable Launch Vehicle – Technology Demonstrator (RLV-TD)

 January 11, 2019     1 comment   

RLV-TD 

Reusable Launch Vehicle – Technology Demonstrator (RLV-TD) is one of the most technologically challenging endeavors of ISRO towards developing essential technologies for a fully reusable launch vehicle to enable low cost access to space. The configuration of RLV-TD is similar to that of an aircraft and combines the complexity of both launch vehicles and aircraft. The winged RLV-TD has been configured to act as a flying test bed to evaluate various technologies, namely, hypersonic flight, autonomous landing and powered cruise flight. In future, this vehicle will be scaled up to become the first stage of India’s reusable two stage orbital launch vehicle.
RLV-TD consists of a fuselage (body), a nose cap, double delta wings and twin vertical tails. It also features symmetrically placed active control surfaces called Elevons and Rudder. This technology demonstrator was boosted to Mach no: 5 by a conventional solid booster (HS9) designed for low burn rate.  The selection of materials like special alloys, composites and insulation materials for developing an RLV-TD and the crafting of its parts is very complex and demands highly skilled manpower. Many high technology machinery and test equipment were utilised for building this vehicle.
Objectives of RLV-TD:
  • Hypersonic aero thermodynamic characterisation of wing body
  • Evaluation of autonomous Navigation, Guidance and Control (NGC) schemes
  • Integrated flight management
  • Thermal Protection System Evaluation



Achievements:
RLV-TD was successfully flight tested on May 23, 2016 from SDSC SHAR Sriharikota validating the critical technologies such as autonomous navigation, guidance & control, reusable thermal protection system and re-entry mission management.
Mission Parameters
RLVTD Vehicle Configuration 
Vehicle Configuration
Mission Profile 
 Mission Profile

Tracking of RLVTD
     Tracking of RLV-TD Mission

Related Images

RLV-TD Lift offRLV-TD Lift offRLV-TD Lift offRLV-TD Lift offRLV-TD LaunchRLV-TD LaunchRLV-TD LaunchRLV-TD LaunchRLV-TD LaunchRLV-TD Trial mock-Up at SHAR
  • Share This:  
  •  Facebook
  •  Twitter
  •  Google+
  •  Stumble
  •  Digg
Email ThisBlogThis!Share to XShare to Facebook
Newer Post Older Post Home

1 comment:

  1. ReddyJanuary 11, 2019 at 7:41 PM

    GOOD

    ReplyDelete
    Replies
      Reply
Add comment
Load more...

Popular Posts

  • Trending MARS ORBITER MISSION
    Trending MARS ORBITER MISSION Marking India's first venture into the interplanetary space, MOM will explore and observe Mars su...
  • FUTURE GSLV-Mk III / Chandrayaan-2 Mission
    FUTURE GSLV-Mk III / Chandrayaan-2 Mission Chandrayaan-2 , India's second mission to the Moon is a totally indigenous mission comp...

Recent Posts

LightBlog

Categories

Chandrayaan-2 has three modules namely Orbiter India’s second lunar mission Lander (Vikram) & Rover (Pragyan).

Unordered List

recentposts

Pages

Text Widget

Blog Archive

  • Home
  • About
  • Contact
Powered by Blogger.
  • Post Style
  • Feature
  • _Gadget
  • _Mobile
  • Pages
  • Categories
  • Buddypress
  • Download

Search This Blog

About Me

My photo
Reddy
View my complete profile

Contact Form

Name

Email *

Message *

  • Home
  • Home
  • Features
  • _Multi DropDown
  • __DropDown 1
  • __DropDown 2
  • __DropDown 3
  • _ShortCodes
  • _SiteMap
  • _Error Page
  • Video Documentation
  • Documentation
  • Download this template

Tags

Chandrayaan-2 has three modules namely Orbiter India’s second lunar mission Lander (Vikram) & Rover (Pragyan).

Tags

Chandrayaan-2 has three modules namely Orbiter India’s second lunar mission Lander (Vikram) & Rover (Pragyan).

Facebook

Home Top Ad

Responsive Ads Here

Business

banner image

recent posts

banner image
Responsive Ads Here

Comments

Random Posts

randomposts

Recent Posts

recentposts

Popular Posts

  • Trending MARS ORBITER MISSION
  • FUTURE GSLV-Mk III / Chandrayaan-2 Mission
    FUTURE GSLV-Mk III / Chandrayaan-2 Mission

Sample Text

Copyright © Indian Space Research Organization | Powered by Blogger
Design by Hardeep Asrani | Blogger Theme by NewBloggerThemes.com | Distributed By Gooyaabi Templates