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We are honored to announce that the Indian Institute of Space Science and Technology (IIST) has been -
𝐈𝐈𝐒𝐓 𝐚𝐧𝐝 𝐌𝐢𝐜𝐫𝐨𝐠𝐫𝐚𝐯𝐢𝐭𝐲 𝐑𝐞𝐬𝐞𝐚𝐫𝐜𝐡 Group Captain Shubhanshu Shukla, an Indian Air Force pilot and -
ISAT2 – A nanosat technology mission for demonstrating IIST cold gas thruster and Topside ionosonde -
The IIST ground station can operate in the UHF for telecommand and telemetry of the INSPIRESat-1 at
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Small-spacecraft Systems and PAyload CEntre (SSPACE) is an interdisciplinary centre involved in the
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The student and faculty team of Small-Spacecraft Systems and Payload Centre (SSPACE), IIST has -
Dr. V.Seena, Anju Sebastian, Dr Naveen Kadayinti: Closed Loop In-Plane Movable Suspended Gate FET
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Dr. Palash Kumar Basu and his group in Dept of Avionics is conducting research to develop -
Design and realization of Dual band (S-X and S-Ka) ground station feed antenna for LEO (Low Earth
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The IoT-enabled biomedical wearable leverages the power of the Internet of Things (IoT) to transform
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ARIS (Advanced Retarding Potential Analyser for Ionospheric Studies) is an ionospheric plasma and -
Hard coatings for improving the lifetime of ballbearings in ISRO Spacecrafts: Under MoU with ISRO -
Small-spacecraft Systems and PAyload Centre (SSPACE) is a center where the faculty members from -
M/s Vashishtha Research Pvt Ltd., the startup company incubated under Department of Aerospace -
M/s Vashishtha Research Pvt Ltd., the startup company incubated under Department of Aerospace -
Bright Quantum Squeezed Light in IIST Quantum squeezing refers to quantum noise reduction beyond the -
A common aerosol sampling inlet system (ASIS) is designed and developed at IIST to sample the -
Random positioning machine (RPM) as a ground based microgravity simulating platform was designed -
InspireSat-1 was successfully launched on board the PSLV C52 mission on February 14, 2022 and is -
Pslv-In-orbitaL Obc and Thermals (PILOT), is a payload designed for the fourth (and final) stage of -
With the goal of in-situ radiation dosimetry, SSPACE (Small-spacecraft Systems and PAyload CEntre) -
The invention is a closed loop MEMS Accelerometer implemented using suspended gate field effect
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