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ADITYA-L1

Aditya L1 shall be the first space based Indian mission to study the Sun. The spacecraft shall be placed in a halo orbit around the Lagrange point 1 (L1) of the Sun-Earth system, which is about 1.5 million km from the Earth. A satellite placed in the halo orbit around …

Aditya-L1

Overview

Destination: Heliocentric L1
Mission: Heliophysics

Heliocentric L1 Satish Dhawan Space Centre Second Launch Pad Satish Dhawan Space Centre, India

Aditya L1 is an Indian solar observation satellite to be placed at the Sun-Earth Lagrangian point L1. The major scientific objectives of the mission are to achieve a fundamental understanding of the physical processes that heat the solar corona, accelerate the solar wind and produce Coronal Mass Ejections (CMEs). Originally the mission design started as a small LEO satellite carrying only a coronagraph as a payload. In order to get the best science from the Sun, continuous viewing of the Sun is preferred. A Satellite placed in the halo orbit around the L1 Lagrangian point of the Sun-Earth system has the major advantage of continuously viewing the Sun without any occultation/ eclipses.

Updates

Cosmic_Penguin • Sept. 2, 2023, 7:31 a.m.

Launch success.


Cosmic_Penguin • Sept. 2, 2023, 6:20 a.m.

Liftoff.


LL2 • Sept. 2, 2023, 5:46 a.m.

Livestream has started


hitura-nobad • Aug. 28, 2023, 10:52 a.m.

Setting T-0 to 06:20 UTC and Status to GO


Cosmic_Penguin • Aug. 10, 2023, 12:47 a.m.

Added launch date and time per NOTAMs.


PSLV-XL

Family:
Configuration: XL

PSLV-XL is the upgraded version of Polar Satellite Launch Vehicle in its standard configuration boosted by more powerful, stretched strap-on boosters with 12 tonne propellant load. Weighing 320t at lift-off, the vehicle uses larger strap-on motors (PSOM-XL or S12) to achieve higher payload capability. On 29 December 2005, ISRO successfully tested the improved version of strap-on booster for the PSLV. The first use of PSLV-XL was the launch of Chandrayaan-1 by PSLV C11. The payload capability for this variant is 1,800 kg to SSO.

Specifications
  • Stages
    4
  • Length
    44.0 m
  • Diameter
    2.8 m
  • Fairing Diameter
  • Launch Mass
    320.0 T
  • Thrust
Family
  • Name
    PSLV-XL
  • Family
  • Variant
    XL
  • Alias
  • Full Name
    PSLV XL
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity
    1800.0 kg

Indian Space Research Organization

Indian Space Research Organization

(ISRO)

Chairman: S. Somanath Founded: 1969 Successes: 78 Failures: 13 Pending: 19

Agency Type:

The Indian Space Research Organisation (ISRO) is the space agency of the Government of India headquartered in the city of Bangalore. Its vision is to "harness space technology for national development while pursuing space science research and planetary exploration."

INFO WIKI

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