Aerospace
Welcome to our Aerospace Project Showcase, where innovation meets confidentiality. Explore our highlighted projects, such as the Rocket, Cubesat and UAV for advanced surveillance and our breakthrough in lightweight aerospace components. While some projects remain confidential, these examples reflect our commitment to pushing the boundaries of technology in the aerospace industry. Contact us for more details and potential collaborations.
01
3d Printed Sounding Rocket
Despite the increase of rainfall globally with the climate change, the large rivers are drying out. Less water in the river means less water supply to the cities and agricultural land, and indeed need more water for the dry soil for the farm.Eventually there is a need for more water than available. Cloud seeding has become one of the appealing methods across the globe for countries to accomplish the need of water. The cost involved in cloud seeding is gigantic. The implementation of cloud seeding with the 3D Printed Sounding Rocket can reduce ample amount of cost. This can also be used concurrently for agricultural surveying, in supplementary can help in research field on farm. Cloud seeding is enhancing the natural precipitation in clouds with the help of seeding agent, i.e., dry ice and silver iodide. Silver iodide is used for its similar molecular structure with water. 3D Printed Sounding Rocket is built with biodegradable material, PLA (Poly Lactic Acid), which contribute in reducing average cost of the cloud seeding process. On the basis of the experiment, the thrust requirement for 50 kg of rocket would be around 4521.3 N. Rocket travelling range is up to 48 to 145Km and carries payload of 10 to 100Kg as per the capability of designed rocket. Being first in India to evolve cloud seeding process with complete 3D Printed Sounding Rocket can have a great impact on Indian Economy.
02
High Speed Expandable Aerial Target Vehicle
A High-Speed Expandable Aerial Target Vehicle is an unmanned aircraft designed for use in military training exercises, particularly for anti-aircraft weapon testing. These vehicles are characterized by their ability to simulate the speed, maneuverability, and radar cross-section of real-world threat aircraft. Typically launched from the ground or air, these target vehicles can mimic the flight characteristics of various types of aircraft, providing realistic and dynamic training scenarios for air defense systems. Their expandable nature allows for cost-effective training as they can be recovered and reused, making them valuable tools in enhancing the readiness and effectiveness of military forces.
03
Liquid Rocket Propulsion System
The liquid rocket propulsion system for OrbitX utilizes a combination of liquid hydrogen and liquid oxygen as propellants, ensuring efficient combustion in the combustion chamber. The engine incorporates a sophisticated thrust vector control system for precise orientation during orbital maneuvers. Regenerative cooling mechanisms prevent overheating, while turbopumps pressurize and feed propellants into the combustion chamber. Stage separation is facilitated for multi-stage missions, and guidance and control systems enable accurate trajectory adjustments. The launch vehicle design integrates considerations for structural integrity and aerodynamics, with a payload fairing providing protection during ascent. Small thrusters or RCS allow for fine-tuned orbit adjustments in space. Thorough testing and validation ensure safety and reliability, making this liquid rocket propulsion system a key component in achieving successful orbital missions for OrbitX.
04
Rocket System Design for Unlocking of Parachute
The rocket system for unlocking a parachute is equipped with a precision deployment mechanism triggered by an altitude sensor. Whether utilizing pyrotechnics or mechanical systems, the design emphasizes safety redundancies to prevent inadvertent releases. Aerodynamic considerations are paramount to ensure stable parachute deployment. Integrated seamlessly with the rocket structure, the system accommodates various parachute types and employs an electronic control unit for precise timing. Rigorous testing and validation procedures guarantee reliability under diverse conditions. An emergency override allows manual triggering if sensors fail. With a focus on compactness and lightweight design, the system minimizes impact on rocket performance. Real-time monitoring capabilities enable mission control intervention, ensuring adaptability to different mission profiles. This versatile design is suitable for diverse aerospace applications, providing a reliable means for controlled parachute descent.
05
Design and Development of Active Rocket Attitude Control System and Recovery System for a Drop test Demonstration of RLV (Reusable Launch Vehicle).
The active rocket attitude control system for a Reusable Launch Vehicle (RLV) drop test includes a Reaction Control System (RCS), gyroscopes, and accelerometers for precise orientation. Recovery involves a staged parachute system with drogue chutes for stabilization and main chutes for final descent. Altitude and descent sensors optimize parachute deployment. Aerodynamic design ensures stability, and sophisticated control algorithms manage dynamic changes. Telemetry and communication systems allow real-time monitoring and intervention. The structure is reinforced for stress resistance, and an efficient power system supports avionics. Simulation and testing validate system functionality, while an emergency abort system provides a fail-safe. Post-flight data analysis informs improvements, and regulatory compliance and safety protocols ensure a secure drop test demonstrating the RLV's capabilities.
06
Designed and Development of Wind Tunnel
The wind tunnel is designed with a closed-loop structure featuring a transparent test section for aerodynamic simulations. Powered by a high-capacity fan or compressor system, it allows precise control of wind speeds, pressure, and temperature. The test section includes instrumentation like pressure taps and pitot tubes for data collection during experiments. A versatile model mounting system ensures stability and reproducibility. Flow straighteners and screens eliminate turbulence, while adjustable features enable a range of aerodynamic studies. A robust data acquisition system captures real-time data for comprehensive analysis of forces and moments. Safety features, emergency shutdown systems, and airflow visualization techniques maintain secure testing conditions. The wind tunnel integrates pressure and vacuum systems to simulate diverse conditions, and turbulence generators replicate real-world scenarios. Consideration for acoustic issues, regular calibration protocols, and user-friendly interfaces enhance its usability, ensuring adaptability for future upgrades. This holistic approach makes the wind tunnel a valuable tool for studying aerodynamics in various fields.
07
Implementing the 3d Printed Active Rocket Attitude Control System for a Simple Drop test Demonstration of Reusable Launch Vehicle
Implementing a 3D-printed active rocket attitude control system for a simple drop test of a Reusable Launch Vehicle involves designing components using CAD, selecting suitable 3D-printable materials, and integrating sensors and control systems during printing. The process includes wind tunnel testing, assembling components, and verifying structural integrity. Incorporate 3D-printed housings for electronics, altitude sensors, and parachute deployment systems. Execute the drop test, monitoring the active attitude control system's performance and parachute deployment. Analyze collected data to assess system effectiveness. Iteratively improve 3D-printed components based on insights from the test. Thorough documentation of the design, manufacturing process, and test results is crucial for future development and regulatory compliance. This approach leverages additive manufacturing's flexibility for rapid prototyping in aerospace applications.
08
Design and Development of Pesticide Spraying Drone for Arecanut with Variable Vector Nozzle
The pesticide spraying drone for arecanut cultivation features a lightweight design with a variable vector nozzle for precise pesticide dispersion. Equipped with GPS navigation and collision avoidance sensors, the drone follows an automated flight path, optimizing coverage in arecanut plantations. Remote monitoring provides real-time feedback, while smart battery management ensures extended flight durations. The drone is weather-resistant and designed for easy maintenance, adhering to regulatory standards. Training programs support operators, and environmental impact considerations minimize chemical drift. Cost-effective manufacturing processes aim for widespread adoption. Field testing and iterative improvements based on user feedback solidify the drone's efficiency, addressing the unique needs of arecanut farmers in a comprehensive and sustainable manner.
09
Underwater UAV Technology by the combination of underwater electronics in combination with aero and hydrodynamic technology
The integration of underwater electronics with aero and hydrodynamic technology in Underwater Unmanned Aerial Vehicles (UUVs) involves a hybrid design with aero-hydrodynamic bodies for efficient movement in air and water. A versatile propulsion system facilitates seamless transitions between environments. Specialized underwater electronics, adaptive control systems, and dual-mode sensors enable effective navigation and data collection in both air and water. Energy harvesting technologies ensure sustained operations during aerial and underwater missions. Advanced communication systems support real-time data transfer during transitions. Autonomous navigation algorithms reduce the need for constant human intervention. The UUV is designed for multi-mission capabilities, catering to applications such as environmental monitoring and surveillance. Materials are chosen for durability and corrosion resistance in diverse environments. Rigorous testing in simulated conditions validates performance and refines design. A user-friendly interface aids mission planning, making the UUV applicable in security, defense, and environmental research, offering a unique and adaptive solution for complex operational scenarios.
10
Cubical satellite for Campus Monitoring
A cubical satellite designed for campus monitoring features a compact, versatile design for seamless integration. Equipped with a multi-sensor payload, including cameras and environmental sensors, it enables comprehensive surveillance. Robust communication systems facilitate real-time data transmission to ground stations. Solar panels and energy storage ensure continuous operation, even during periods without direct sunlight. Optimized for low Earth orbit, the satellite conducts frequent passes over the campus for regular data collection. Autonomous operation capabilities and on-board data analysis algorithms enhance efficiency. Security features prevent unauthorized access, and wireless network integration fosters communication with campus devices. A real-time monitoring dashboard provides live updates to campus authorities. Environmental sensors contribute to sustainability efforts, while emergency response support enhances campus safety. The satellite's educational component engages students in STEM initiatives. Cost-effective manufacturing allows for the deployment of multiple satellites, offering a comprehensive solution for continuous campus monitoring.
11
Cubesat for Weather Detection.
A CubeSat designed for weather detection is a compact satellite equipped with instruments for atmospheric monitoring. Payload includes spectrometers, radiometers, and thermal sensors for real-time data on temperature, humidity, and atmospheric composition. Remote sensing capabilities enable global weather pattern observation. Integration of GPS ensures precise location determination. Reliable communication systems facilitate data transmission to ground stations. Solar panels provide sustainable power during orbit. Optimal low Earth orbit (LEO) allows frequent passes over varied regions. Onboard data processing minimizes bandwidth needs. Miniaturized weather instruments fit within CubeSat constraints, while a deployable antenna enhances communication range. Real-time weather mapping algorithms create dynamic models. An educational outreach component engages students, and collaboration with meteorological agencies enhances weather prediction accuracy. Cost-effective manufacturing allows for the deployment of multiple CubeSats, contributing to improved global weather detection capabilities.
11
Design and Development of ground station for Cubesat
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The ground station for CubeSats is equipped with a tracking antenna system for continuous communication with satellites in various orbits. It features radio frequency (RF) equipment, a tracking and telemetry system for real-time monitoring, and data reception capabilities for mission telemetry and scientific data. A command and control center facilitates mission planning, execution, and security protocols to safeguard sensitive data. The ground station supports remote operations, allowing flexibility and efficiency in satellite control. Automated tracking mechanisms adapt to CubeSat movements, ensuring constant communication. Data storage and archiving systems retain historical mission data, while a user-friendly interface streamlines monitoring and control. Integration with mission control software enhances overall operational efficiency. Power backup systems and reliable network connectivity ensure uninterrupted communication. The ground station serves as a training facility for operators, offering remote diagnostic capabilities for issue resolution and contributing to the success of CubeSat missions.
12
Vertical takeoff and landing Aircraft.
A Vertical Takeoff and Landing (VTOL) aircraft is designed with a multicopter configuration or tilt-rotor/tilt-wing design, allowing for precise vertical lift and efficient transition to horizontal flight. Powered by an advanced propulsion system, such as electric or hybrid, it ensures both performance and environmental efficiency. Autonomous navigation capabilities, including automated takeoff and landing, enhance operational ease. The aircraft's design accommodates diverse applications with ample payload capacity, such as cargo transport, surveillance, or passenger services. Noise reduction technologies address acoustic challenges, making it suitable for urban environments. Sturdy and retractable vertical landing gear ensures stability during descent. Emergency landing systems add an extra layer of safety. Optimization of range and endurance is achieved through efficient aerodynamics and propulsion systems. A modular design facilitates maintenance, while regulatory compliance ensures safe and legal operations. Adaptability to various environments, from urban to remote areas, broadens its utility, and a commitment to continuous innovation keeps the VTOL aircraft at the forefront of technological advancements.
12
Vertical Takeoff and Landing Unmanned Aerial Vehicle.
A Vertical Takeoff and Landing (VTOL) Unmanned Aerial Vehicle (UAV) is designed with a multicopter configuration for precise vertical lift and efficient transition to horizontal flight. Compact and lightweight, it employs an electric propulsion system for reduced noise and environmental impact. Advanced flight control systems ensure stability during takeoff, landing, and transitions. Autonomous navigation capabilities allow for independent task execution. Real-time telemetry and communication systems enable remote control and data transmission. The UAV accommodates diverse payloads for applications such as surveillance and mapping. Obstacle avoidance sensors enhance navigation in complex environments, while weather-resistant features ensure operational versatility. Reliable vertical landing gear supports stable landings in various terrains. Emergency landing systems contribute to safety in critical situations. Regulatory compliance and modular components facilitate maintenance and ensure legal operations. Continuous software updates keep the UAV technologically current and adaptable to evolving needs.