PSLV-XL | EOS-09 (RISAT-1B)
18/04/2025 Ultimo aggiornamento
Chairman: V. Narayanan Amministratore
To Be Determined Status

PSLV-XL | EOS-09 (RISAT-1B)

Satish Dhawan Space Centre, India

Orbital Launch Attempt Count: 6953

Location Launch Attempt Count: 99

Pad Launch Attempt Count: 62

Agency Launch Attempt Count: 95

Launch Designator:

Net Precision: Month

Weather Concerns:

Fail Reason:

Flightclub URL:

Pad Turnaround: P151DT7H29M45S

Programma

Pad

First Launch Pad
Satish Dhawan Space Centre First Launch Pad

Satish Dhawan Space Centre – SDSC (formerly Sriharikota Range – SHAR),[1] is the primary spaceport of the Indian Space Research Organisation (ISRO), located in Sriharikota, Andhra Pradesh.

Rocket

[AUTO] PSLV-XL - image
PSLV-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.

Full Name: PSLV XL

Maiden Flight: 2008-10-22

Total Launch Count: 26

Successful Launches: 25

Failed Launches: 1

Mission

Mission Name: EOS-09 (RISAT-1B)

Type: Government/Top Secret

Description: RISAT-1B is the third in the series of radar imaging RISAT-1 satellites of ISRO using an active C-band SAR (Synthetic Aperture Radar), providing all-weather as well as the day-and-night SAR observation capability in applications such as agriculture, forestry, soil moisture, geology, sea ice, coastal monitoring, object identification, and flood monitoring, in addition to military surveillance. The RISAT-1 series is developed, manufactured and integrated by ISRO. The 3-axis stabilized spacecraft bus consists of a hexagonal prism shape build around a central cylinder. Most of the spacecraft subsystems and the payload are integrated in the prism structure and the central cylinder. The solar panels and some subsystems are mounted on the cube-shaped section of the spacecraft.

Orbit: Low Earth Orbit

Updates

Cosmic_Penguin

Cosmic_Penguin

2025-04-18T16:07:00Z
https://x.com/TitaniumSV5/status/1913248212325933506

Added launch.