Sam Manekshaw
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Are newer statistics available (2013 & 2014) ??
These details r old one..any one has the latest info on these...RLVNAL India performs Dynamic testing of RLV-TD models
RLV Concept (Credit ISRO)[
Reusable Launch Vehicle is envisioned by ISRO as an alternative to expendable launch vehicles to cut down the cost of space transportation. To achieve this goal, ISRO is currently developing a Reusable Launch Vehicle Technology Demonstrator (RLV-TD) to act as a platform to demonstrate various technologies like
1) hypersonic flight,
2) autonomous landing,
3) flush air data measurements,
4) Re-entry thermal protection systems, etc.
RLV-TD Ascent and Descent configuration models (Credit NAL)
ISRO is utilizing various NAL facilities to perform tests on scaled model of RLV-TD. Dynamic tests were performed by NAL using forced oscillation rig to determine the pitch/yaw damping characteristics of a scaled model of RLV-TD configuration. This will help in building flight stability augmentation system for both ascent and descent configuration of RLV-TD. These tests were carried out in the 1.2 m trisonic wind tunnel facility.
RLV-TD Ascent configuration model in wind tunnel testing at NAL.
RLV-TD Descent configuration model in wind tunnel testing at NAL.
ISRO Air Breathing Propulsion
Extensive CFD analysis has been going on to understand various phenomena that occurs inside scramjet engine in a flight.
CFD Analysis of scramjet inlet @ ISRO.
CFD Analysis of scramjet inlet @ ISRO.
Scramjet Engine Intake CFD flows @ ISRO.
Some pics of PSLVs with shock condensation collar during launch...it's nothing strange, just a regular phenomenon, but
interesting.
Look at the power of the Motor. Flame of the rocket motor is an indicator of that.
The flame of the Mk 3 will be much bigger than this.