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Extending thoughts into space...

"Parikshit is your 'Pariksha'! Learn well, question deeply. Don't take anything for granted. Success will be yours. God Bless, Happy Creating and testing!"
-Wing Commander Rakesh Sharma, First Indian in Space, Visiting Parikshit

The Question guarding our interstellar mission is...

Who are We?

An interdisciplinary undergraduate student satellite team founded in 2013 at Manipal Institute of Technology, India.
Developing a 2U-Class Nanosatellite for launch in an Indian Space Research Organisation (ISRO) vehicle.
We design and develop all subsystems in-house, namely:

Satellite photo
  1. ADCS
  2. ODHS
  3. COMMS
  4. PAYLOAD
  5. EPS
  6. STMS

We have a Thermal Imaging payload with high accuracy, built-in deorbiting mechanism as an experimental payload, designed for a Polar Low Earth Orbit.

Mission: Pushing boundaries of student-led space projects and fostering space engineering expertise in India.

The Cubesat:

  • Primary Payload: Thermal Imaging Camera
    Secondary Payload: Electrodynamic Tether
  • Dimensions: 10x10x22.7 cm
  • Weight: 2.3Kg
  • Altitude: 500km (LEO)
  • Battery: Li-ion 20Wh
  • Actuation System: Reaction Wheel, Torquerods
  • Sensors: Magnetometer, Gyro, Sun Sensors
Orbital Physics and Controls

Attitude Determination and Control Subsystem

The Attitude Determination and Controls subsystem or ADCS is at the heart of the satellite's mission, overseeing crucial aspects, from orbit design to spacecraft orientation. We are responsible for:

RF Electronics, Electromagnetics and Communications

Communications and Ground Stations Subsystem

The Communications and Ground Station Subsystem or COMMS is responsible for the team to establish a communication link between the Ground Station and the Satellite. The subsystem deals with making RF modules, building antennae, data processing and tracking satellites from PAGOS. The main motto is to design the system in such a way that there always exists a strong link with minimal interference.

Electronics

Electronics and Power Subsystem

The Electronics and Power Subsystem or EPS is responsible for the generation, distribution and regulation of power on the satellite. In addition to this, we also design all onboard circuitry and PCBs inhouse.

Firmware, operating system and embedded system

Onboard Data Handling Subsystem

The On-Board Data Handling Subsystem (ODHS) is a critical component of satellite systems, designed to ensure the seamless and orderly functioning of all satellite parts. It plays a vital role in managing the flow of data, maintaining communications, and ensuring the satellite operates smoothly throughout its mission.

Image Processing, AI, and Plasma Physics

Payload Subsystem

Our satellite mission features two innovative Payloads: a thermal imaging camera and an electrodynamic tether, each designed to push the boundaries of space technology.

Mechanical

Structures, Thermals and Mechanisms Subsystem

The mechanical subsystem in Parikshit consists of three segments: Structures, Thermals and Mechanisms. The broad function of this subsystem is to design the body of the satellite and mount all components on it, shielding them well from vibration and excessive temperatures. It manages control of the internal thermal environment at all times and designs mechanisms crucial to the working of components.

Project Management

Administration Subsystem

At the heart of our organization's efficiency lies the Operations and Administration Subsystem. This integral part of our team ensures that all aspects of our digital presence run smoothly, with a focus on the following key areas: