ARIS (Advanced Retarding Potential Analyser for Ionospheric Studies) is an ionospheric plasma and electrostatic instrument developed by IIST for the structural and compositional studies of the

Hard coatings for improving the lifetime of ballbearings in ISRO Spacecrafts: Under MoU with ISRO Inertail Systems Unit (IISU) for developing surface engineering techniques for improving the life and

Small-spacecraft Systems and PAyload Centre (SSPACE) is a center where the faculty members from multiple departments of the institute are actively involved in the development of spacecraft systems for

M/s Vashishtha Research Pvt Ltd., the startup company incubated under Department of Aerospace Engineering IIST (by one of our research students) has successfully developed and delivered a halogen lamp

M/s Vashishtha Research Pvt Ltd., the startup company incubated under Department of Aerospace Engineering IIST (by one of our research students) has successfully developed and delivered a 4 axis

Bright Quantum Squeezed Light in IIST Quantum squeezing refers to quantum noise reduction beyond the standard quantum limit (SQL), the minimum noise limit in classical physics. In IIST, for the first

A common aerosol sampling inlet system (ASIS) is designed and developed at IIST to sample the ambient aerosols to characterize their physical, optical, and chemical properties (Figure 7). The

Random positioning machine (RPM) as a ground based microgravity simulating platform was designed, fabricated and validated. Experiments using biological samples proved that the achieved microgravity

The paper titled “Development of Process Parameters and Tool Path Strategies for Laser Powder Directed Energy Deposition of Axisymmetric Components”, authored by Akhil A I (IIST), V S Sooraj (IIST)

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Memorandum of Understanding was signed between Indian Institute of Space Science and Technology (IIST) Thiruvananthapuram and Indian Institute of Technology (IIT) Palakkad on 19th August 2024 to

The project titled “Generative Design and Topology Optimization Studies on Aerospace Components for Additive Manufacturing”, completed by Mr Aakash Preetham Vadlakunta (Currently Scientist /Engineer

The invention is a closed loop MEMS Accelerometer implemented using suspended gate field effect transistors (SGFET) and the method of fabricating this sensor. This closed loop accelerometer (Closed