Special Sessions
IEEE Space, Aerospace and Defence Conference, SPACE 2025
Semiconductor Technologies : Defence and Space Applications
Cislunar Transport, Guidance, Navigation, and Space Domain Awareness







Abstract
Session Moderator: Ms. Suma Varughese, Director General MED & CoS (Micro Electronic Devices and Computational Systems & Cyber Systems), DRDO
- Present Status of Indigenous Technologies
- Laser Technology
- InP HEMT and THz: launch pad for networking in space
- Infrared Focal Plane Array Technologies-HgCdTe & State of the Art
- High Efficiency III-V Triple junction Solar cell for space application
- Silicon Carbide Devices: Enabling Efficient Power Electronics for a Sustainable Future
- GaN technology for Ka-band: Key challenges and prospects
- Present Status of Indigenous Technologies:
Future defence systems and space technologies focus on the application of information technology and computer networking to get the advantage by using of EO systems in areas like sophisticated 3D visualisation, laser radars, and infrared sensors. This provides the defence forces with a better situational awareness and Improvement of surveillance and military ISR capabilities. Developing these systems require material and device technologies for Tuneable detectors and tuneable sources like QCL, VCSEL, DFB, T2SLbased detectors and APD. Similarly, RF sensors which remains largely concealed and shrouded in secrecy are required to work in higher frequencies with technologies like GaN Ka band and InP based THz sources and detectors. These technologies owing to its broadband operation and enhanced reliability find application in futuristic defense systems. These technologies have begun making inroads into the SatCom market, leveraging high efficiency compared to other materials to enable smaller device sizes, thereby saving valuable space at the system level. Transitioning from L/C/X-bands to Ku/Ka-bands enables higher data rates in mobile satellite communication. SiC power devices and high efficiency solar cells are technologies for green energy required both for defence and space applications. This special session will give insight into all the above mentioned technologies along with the indigenous status. Laser Technology: Dr. Soma S Mahajan:
SSPL Delhi is involved in the development of high power laser diodes. Over the years, various laser diode technologies have emerged including single emitter laser diodes, arrays, stacks and fiber coupled laser diodes (FCLD) in different operational modes and varied output powers employed for defence applications ranging from range finders, dazzelers, proximity fuses, fencing, explosive initiation for detonation etc. Recently, fabrication of indigenous laser diode technology has successfully been established at GAETEC, Hyderabad, a pilot production plant which is now capable of production of single emitter laser diode technology upto 10W (CW) for 976 nm emission. The 10W single emitters serve as the basic building blocks for high power Fiber coupled laser diodes (FCLDs) modules employed for Directed Energy Weapons (DEW) applications and initiation of explosive detonation. These modules with output power upto 100W(CW) emitting at 976 nm have also been developed in collaboration with industry. Communication between various underwater entities like submarine to unmanned underwater vehicle (UUV) is a key area for strategic defence applications in blue-green laser region of spectrum. To cater the strategic demand, SSPL is also working on blue-green laser technology employing InGaN/GaN based multiple quantum well laser structures. Laser diodes emitting at 415 nm with the pulsed power upto 4W have been developed. Apart from this, SSPL is also venturing into single mode technology; development of Vertical Cavity Surface Emitting Laser (VCSEL) and Distributed Feedback (DFB) laser diodes to produce a narrow linewidth and stable output power. These special diodes exhibit wide range of applications including optical communication systems, spectroscopy, sensing and also serve as light sources in quantum sensors and quantum communication for quantum technologies. Recently, the first set of VCSEL devices delivering power of 5mW at 850 nm have been realized. The complete development cycle starting from the procurement of raw epitaxial material to device packaging and testing was successfully carried out at SSPL.InP HEMT and THz: Launch pad for networking in space: Dr. Mahadev Bhat K
With the concept of miniature satellites called CubeSats and networking them in space has the potential to revolutionize the twenty first century with extremely high speed of communication in connecting the world as one, through the space and Internet of space things (IoST). Negligible absorption of THz frequency in space compared to the high molecular absorption in earths atmosphere makes the THz frequency operation very suitable for communication in space compared to ground-based applications. Very high bandwidths available in these frequency range also makes high speed data transfer possible. High Electron Mobility Transistors (HEMTs) fabricated on InP Substrate with InxGa1-xAs (x varying from 0.53 to 1) as channel has made this as reality with cut of frequency reaching close to 1THz. Extremely high electron mobility and electron saturation velocity of these devices make them the best suitable candidate for low noise applications as well. with low DC power consumptions and high frequency response make them aptly suitable candidates for CubeSats. Having said that, achieving the THz performance from these devices is extremely challenging with gate lengths very low gate lengths. Exploring various aspects of device technology like material layer engineering, device topological engineering and device fabrication engineering simultaneously is essential to extract the best performance from these devices. Some of the technological challenges involved will be covered in this technical presentation.
Infrared Focal Plane Array Technologies-HgCdTe & State of the Art
Infrared sensor arrays are of high importance for a variety of defence, scientific, and commercial applications. An important requirement for defence surveillance systems is a sensor that can provide all condition vision. IR sensors fulfil this criterion of vision through fog, haze, dust, smoke and night, since they sense the thermal energy emitted by objects as a function of their temperature and emissivity. Other requirements are high sensitivity, fast response to scene changes, thermal stability and ability to tune to various IR windows. Mercury Cadmium telluride (HgCdTe) based semiconductor photon detectors offer all the listed advantages for IR detection. Competing technologies in mid wave infrared (MWIR) and long wave infrared (LWIR) are InSb, antimonide based type II super lattices and quantum well infrared photodetectors (QWIPS). Shortwave infrared (SWIR) sensors are made from HgCdTe and InGaAs materials. Dual band, multi-color and hyperspectral imaging are the recent applications of III generation sensors where HgCdTe and T2SL material systems are commercially viable. Present work reports the development of HgCdTe MWIR photodiode arrays with 15µm pitch in 384×288 and 640×512 format. The FPA package consists of a two-dimensional photovoltaic infrared detector array hybridized with a Si-CMOS based Readout Integrated Circuit (ROIC) using indium bumps. The detector array performs the function of IR signal detection and ROIC consists of signal processing circuitry which collects the signal from individual detector elements and integrates the output signal to form an image. The two-dimensional detector array is fabricated using Hg1-xCdxTe semiconductor material. MCT (Hg1-xCdxTe) epilayers with a composition of x= (0.285-0.295)±0.0005 corresponding to a cut-off wavelength of ~4.8-5.4µm at 89 K are used. The epilayers are grown in-house by LPE technique on CZT substrate. The fabrication steps for photodiode array includes common contact formation, boron implantation for junction formation, p/n-contact etching of diodes, passivation of diodes and finally the indium bump growth to provide metal contact on individual diode pixels and ROIC. The ROIC and detector array are flip-chip bonded using FCB machine. This is followed by backside thinning, antireflection (ARC) coating, wire bonding on Dewar, cooler integration and testing. The technology for IR Focal Plane Array (IRFPA) fabrication and integration is fully developed at SSPL and thermal images of room temperature scenes have been demonstrated.- High Efficiency III-V Triple junction Solar cell for SPACE Application: Dr. Akhilesh Pandey:
III-V Triple junction solar cell-based devices are showing great attention world-wide due to its wide applications in spacecraft and satellite. In the space sunlight is the only high-volume energy source available and are being used to convert light energy into the electrical power. The electrical power generated by solar panel provide the power to the space craft in all phase of life. The smallest unit of the panel is the solar cell which are connected either in series or parallel or both to increase the power which are being utilized in the space craft. Usually normal solar cell (Si, CdTe based) cannot used in the space due to moderate efficiency, limited spectral coverage and availability of high radiation. The III-V arsenide and phosphide based solar cells exhibit several advantages as compared to other solar cells in terms of cost, weight, efficiency and radiation resistance. III-V based solar cell are the best suited in space satellites/space craft. III-V triple junction solar cell (TJSC) structure (InGaP/InGaAs/Ge) consist of three sub cell of band gap 1.88 eV (top cell), 1.4 eV -InGaAs (middle cell), 0.67eV-Ge (bottom cell). To enhance the efficiency three single sub solar cells are added in tandem manner with the help of tunnel junction. III-V multi-junction solar cells technology offers high efficiencies as compared with traditional solar cells and have been used effectively in space applications, concentrated photovoltaics, unmanned aerial vehicle, solar powered drones etc. In this presentation lattice matched III-V triple junction solar cell (LM-TJSC) structure consist of three sub cells {InGaP (1.88eV)/InGaAs (1.4eV)/Ge (.67eV)} integrated with the highly doped tunnel junction grown by MOCVD technique have been analysed structurally and electrically. Structurers are characterized using High resolution x- ray diffraction (HRXRD), planer/cross-sectional FE-SEM and Secondary Ion mass spectroscopy (SIMS) techniques. In the (TJSC) structure layer sequence, layer thickness and doping were determined by SIMS as well as FESEM techniques. Layers composition, strain and substrate offset angle was determined by HRXRD. The TJSC structure (determined by the above characterization) have been used to fabricate as a solar cell with the the photo conversion efficiency ~ 27-28% under AM1.5 condition. The extracted parameters of the solar cell structure have also been used in the simulation study of the TJSC. The structural, electrical characterization and simulation study of the TJSC structure has been presented and it will be very useful to fabricate the high efficiency space solar cell devices. - Silicon Carbide Devices: Enabling Efficient Power Electronics for a Sustainable Future: Dr. Rupesh Kumar Chaubey
Silicon carbide (SiC) electronics is transforming various industries with its versatility. Its temperature resilience and power efficiency make it ideal for aerospace applications, particularly in avionics and propulsion systems, where it enables aircraft to perform better while reducing weight. The defense sector also benefits from SiC’s capabilities, which support mobile artillery and armored transport. Additionally, SiC-based electronics are enhancing electric vehicles by providing efficient and reliable power management, a crucial aspect in this rapidly evolving transportation sector. Furthermore, SiC electronics are being utilized in renewable energy systems, such as solar and wind power, for remote installations, and are also improving the performance of heavy machinery in demanding environments. Overall, SiC technology is contributing to increased operational readiness, better energy efficiency, and lower maintenance costs across these diverse fields. - GaN technology for Ka-band: Key challenges and prospects: Robert Laishram
The increasing demand for high frequency, high linearity, and cost-effective high-power amplifier (HPA) solutions at Ka-band frequencies is a key driving force behind the rapid progress in the development of GaN Ka-band HEMT RF devices. The ability of GaN technology to meet the size, weight, and power (SWaP) constraints is one of its most transformative strengths in meeting the demands of strategic systems, military radars, 5G/6G systems. However, before the full potential of the GaN can be exploited, several critical issues related to the device design, epi-structure and fabrication challenges need to be addresses. The need to aggressive scale the gate length mitigating the adverse issues related to short-channel effects, gate leakage and parasitic capacitances remains a major challenge. The talk will focus on the future prospects of this critical technology, key challenges and briefly touch upon the journey at SSPL to indigenously develop this technology.
Bio-sketch for Speakers:

GD, CGDG, VSSC
Dr. Gopal Jee joined as scientist/engineer ‘SC’ at Vikram Sarabhai Space Centre, ISRO in June 1999. Currently he is holding the post of Group Director of Control and Guidance Design Group (CGDG) of CGSE entity. He graduated from National Institute of Technology (MNREC), Allahabad, India in 1997. Then he did Post-Graduation from Indian Institute of Technology, Delhi, India in Control Engineering and Instrumentation. He completed PhD in Department of Aerospace Engineering, Indian Institute of Technology, Bombay in 2010. His main area of work is Flight control law design for various launch vehicles including Reusable Launch Vehicle (RLV). He mainly contributed for the autopilot design of reusable launch vehicle, crew module control and test vehicle control for testing crew escape system. He won ISRO’s young scientists merit award for the year 2007 in appreciation of his contribution to the Indian space program in launch vehicle avionics area. He also won a few best paper awards in various international conferences. He has two journal publications and about 43 conference papers to his credit and is a reviewer of many international journals. He is a life member of Systems Society of India, Aeronautical Society of India and Indian Society of Systems for Science and Engineering. His current research interests are in Control law design for air-breathing propulsion system and Integrated guidance and control law design for reusable launch vehicles.

GD, CASG, VSSC
BIJU PRASAD B obtained his PhD in Mechanical Engineering from CUSAT, M.E. in Aerospace Engineering from Indian Institute of Science, Bangalore and B-Tech in Mechanical Engineering from College of Engg. Trivandrum, University of Kerala. Presently he is Scientist/Engineer ‘G’, and Group Director, Control Actuation Systems Group, ESAE, VSSC ISRO. He joined VSSC in 1995 and worked in the design and development of Fault tolerant Actuators and sensors for the thrust vector control system and mixture ratio control system of satellite launch vehicles such as LVM3, HRLV, PSLV, SSLV, RLV and Gaganyaan (manned mission), Landing Gear systems for Reusable Launch Vehicles, Robotic systems for space application. He is also, Associate Project Director, RLV ORV (Landing gear systems) and Deputy Project Director, LVM3 (Control systems). He holds one patent on linear electromechanical actuator. He is a recipient of team excellence award for the development of LVM3. His Areas of interest include Fault Tolerant Actuators, Mechanisms and Robotics.

Group Director,
RFSG/AVN, VSSC
Lal M J, Scientist/Engineer G is Presently holding the post of Group Director, RF Systems Group, Avionics Entity, VSSC. He Has 33 years of experience in Instrumentation, Development of Data Acquisition Systems, Development RF Systems and Project Management. He Graduated in Electronics and Communication from University of Kerala in 1991. He Joined Vikram Sarabhai Space Centre in 1992 as Test Engineer in Integrated Structural Dynamic Test Facility, Structures Entity. He completed his Post graduation in Telecommunication from Indian Institute of Science in 2001. He Worked in RF Systems area 2001-2017 and Moved over to core PSLV Project as Deputy Project Director, Electrical Integration and Checkout Systems in 2017. He was Associate Project Director of PSLV 2019-2023 and Vehicle Director, PSLV-C57/Aditya-L1 Mission.

EPG, VSSC
Sheena Abraham, Scientist/Engineer ‘G’ from Vikram Sarabhai Space Centre is the Group Director of Electronics Production Group of Electronics Systems and Actuators entity. She took her BTech in Electronics and Communication from College of Engineering, Trivandrum in 1994 and MTech in Electronics Design and Technology from Indian Institute of Science, Bangalore. She joined VSSC in 1995 and has 30 years of experience in different fields like design and miniaturization of sensors, design and development of Data Acquisition systems, development of miniaturization technologies, production of Avionics Packages. She has developed advanced and miniaturized sensors like MEMS Acoustic sensor, MEMS based Smart Pressure Sensor, Piezoelectric Vibration Sensor and MEMS Rate Sensors. The sensors developed by her have flown in different Launch Vehicles. The MEMS acoustic sensor developed by her is the first indigenously developed MEMS sensor to be flight tested in an Indian Launch Vehicle. A patent has been granted for her invention “MEMS based sensor for measuring acoustic pressure”. She has also contributed a lot in the area of Electronic Packaging technologies like Hybrid Micro circuits and Surface Mount Technology. She has set up and qualified a SMT Machine soldering line in VSSC for the reflow soldering of all Avionics Surface Mount assemblies. She is at present responsible for the realization of Avionics packages for all operational Launch Vehicles like PSLV, GSLV, LVM3 and development vehicles including Gaganayaan through external industries as well as through in-house facilities. She has taken a lead role in enabling many external industries for the production of Avionics Packages to meet ISRO launch manifesto. She has been awarded ISRO Team award in the year 2017 for “PSLV C37 with 104 Satellites-Multi satellite integration mission operation”. She has won the Institution of Electronics and Telecommunication Engineers (IETE) B V Baliga Memorial Award 2020 for her outstanding contribution in the field of Electronics & Telecommunication with emphasis on R&D and industrial development during the past 10 years. She is a Fellow of IETE.
Bio-sketch for Speakers:

Dr. Maruthi Akella is a professor in Aerospace Engineering and Engineering Mechanics at UT Austin where he holds the Cockrell Family Endowed Chair in Engineering. He is founding director for the Center for Autonomous Air Mobility and faculty lead coordinator for the controls, autonomy, and robotics area at UT Austin. His research encompasses coordinated systems, learning, adaptation, and vision-based sensing. His research group contributed for the onboard guidance algorithm for the Intuitive Machines IM-1 mission – the first U.S. moon landing in more than 50 years since the Apollo era. The major impacts of Dr. Akella’s work have been recognized through the AIAA Mechanics and Control of Flight Award, the AAS Dirk Brouwer Award, the IEEE-CSS Award for Excellence in Aerospace Control, and the Judith Resnik Space Award from the IEEE Aerospace and Electronic Systems Society. Dr. Akella is Editor-in-Chief for the Journal of the Astronautical Sciences and a Fellow of the AIAA, IEEE, and AAS. In October 2024, the International Astronomical Union designated asteroid number 5376 – a nearly 5-mile diameter-sized minor planet from the main asteroid belt – as “Maruthiakella” honoring Dr. Akella’s contributions to “many successful applications in astrodynamics.”

Dr. Roshan Eapen is an assistant Professor of Aerospace Engineering at the Pennsylvania State University. His research interest lies at the intersection of Dynamical Systems Theory, Astrodynamics, and Computational Vision with specific focus on semi-analytic satellite orbit and attitude theories, optimal control of spacecraft, sensor modeling, light-matter interaction, and vision-based navigation. He runs the Computational Astrodynamics Research and Experiments (CARE) lab which host the Penn State University Dynamial observatory (PSUDO), a 0.6m telescope observatory and ground station. He is a JN Tata scholar (2015) and the recipient of the Heep Graduate Fellowship from the Hagler Institute of Advanced Studies.

Dr. Puneet Singla is the Harry and Arlene Schell Professor of the Aerospace engineering at the Pennsylvania State University (PSU). Dr. Singla’s research interface nonlinear dynamics with approximation theory, sensing, uncertainty analysis, and optimal control. He significantly advanced data-driven approaches for a diverse range of highly complex problems such as space domain awareness (SDA), guidance navigation and control (GNC) of hypersonic vehicles, and accurate prediction of toxic plume dispersions. His research related honors include the IEEE AESS’s Judith A. Resnik Award, NSF CAREER award, the AFOSR Young Investigator award, the University at Buffalo’s “Exceptional Scholar” Young Investigator Award and the Texas A&M University’s Young Aerospace Engineering Distinguished Alumni Award in recognition of his scholarly activities. He is IEEE AESS’s distinguished lecturer since 2024. He is a fellow of American Astronautical Society (AAS) and an associate fellow of American Institute of Aeronautics and Astronautics (AIAA).