Rediff India Abroad
 Rediff India Abroad Home  |  All the sections


The Web

India Abroad

Sign up today!

Get news updates:
Mobile Downloads
Text 67333
Article Tools
Email this article
Top emailed links
Print this article
Contact the editors
Discuss this Article

Home > News > Report

ISRO successfully tests Indigenous Cryogenic Stage

November 16, 2007 00:29 IST

Related Articles
Talent crunch: ISRO plans space institute

The Indian Space Research Organisation on Thursday achieved a significant milestone in Mahendragiri, Tamil Nadu, when it successfully tested the indigenously developed Cryogenic Stage, to be employed as the upper stage of India's Geosynchronous Satellite Launch Vehicle.

According to a release, the test was conducted for its full flight duration of 720 seconds at the Liquid Propulsion test facility.

With this test, the indigenous Cryogenic Upper Stage has been fully qualified on the ground. The flight stage was getting ready for use in the next mission of GSLV (GSLV-D3) in 2008.

It may be recalled that a ground test for 480 seconds of the complete stage was conducted on August 4, 2007.

The indigenous Cryogenic Upper Stage was powered by a regeneratively cooled cryogenic engine, which works on staged combustion cycle developing a thrust of 69.5 KN in vacuum.

The other stage systems include insulated propellant tanks, booster pumps, inter-stage structures, fill and drain systems, pressurisation systems, gas bottles, command block, igniters, pyro valves and cold gas orientation and stabilisation system.

Liquid Oxygen and Liquid Hydrogen from the respective tanks were fed by individual booster pumps to the main turbo-pump, which rotates at 39,000 rpm to ensure a high flow rate of 16.5 kg or sec of propellants into the combustion chamber. The main turbine was driven by the hot gas produced in a pre-burner.

Thrust control and mixture ratio control were achieved by two independent regulators. LOX and Gaseous Hydrogen were ignited by pyrogen type igniters in the pre-burner as well as in the main and steering engines.

Apart from the complexities in the fabrication of stage tanks, structures, engine and its sub-systems and control components, CUS employs special materials like Aluminum, Titanium, Nickel and their alloys, bi-metallic materials and polyimides.

Stringent quality control and elaborate safety measures had to be ensured during assembly and integration.

Liquid Propulsion Systems Centre was the lead centre for the development of Cryogenic Upper Stage with the involvement of Vikram Sarabhai Space Centre and other ISRO centres as well as several industries, both in public and private sector.

The successful ground test of the indigenous Cryogenic Upper Stage for the full flight duration had validated the design robustness and performance adequacy for its use in GSLV.