IN-SPACe CanSat Rocketry 2026

Team Vayusat

Pioneering atmospheric innovation and aerospace engineering through advanced CanSat technology and model rocketry. Representing Dayananda Sagar University in ISRO's national arena.

About Get In Touch
Scroll to explore
The Challenge

IN-SPACe Model Rocketry & CAN-7USAT 2026

Organized by the Indian National Space Promotion and Authorization Centre (IN-SPACe) under the Department of Space, this premier competition challenges students to conceptualize, fabricate, and launch model satellites and rockets.

Our dual-track mission focuses on pushing boundaries in two advanced aerospace frontiers:

CAN-7USAT Integration

Designing a high-fidelity Can-sized (7U) satellite limited to 1 kg, loaded with advanced atmospheric data recorders, designed to survive a 1,000m rocket launch and deploy safely.

Precision Ejection & Recovery

Achieving autonomous landing precision and real-time telemetry streaming through customized mechanical deployment and state-of-the-art radio communication link.

Team Vayusat White CanSat Module
7U CanSat White Calibration Module
Team Vayusat Red Branded CanSat Module
7U CanSat Branded Flight Cylinder
Engineering specs

The CanSat Architecture

A state-of-the-art multi-disciplinary satellite sub-system integrating electronics, COMMs, structure, and fluid dynamics.

COMMs & Telemetry

Operating on a specialized 433 MHz RF transceiver network, streaming sensor coordinates and structural health packets in real time directly to our customized ground station dashboard.

  • 1 Hz Packet Rate
  • Custom Helix Antenna
  • Ground Station Software Integration

Electronics & Payload

Powered by a dual-controller architecture on a custom-designed double-sided PCB. Tracks temperature, pressure, relative altitude, acceleration, and GPS coordinates.

  • BMP280 Altitude Sensor
  • MPU6050 Accelerometer/Gyro
  • Dynamic SD-Card Data Mirroring

Structure & Aerodynamics

Built with robust and lightweight 3D-printed composite components. Features impact-absorbent structure cells to shield internal electronics during hard landing deceleration.

  • Carbon-Fiber Reinforced Filament
  • 7U Standardized Form Factor
  • Under 1.0kg Weight Compliance

Controlled Recovery

Utilizes an autonomous dual-parachute recovery system. Deploys a main parachute at optimal ejection altitude, followed by an active landing control mechanism.

  • Servo-Driven Release Mechanism
  • Cross-Parachute Stabilizer
  • Safe descent speed (< 5 m/s)
National Glory

Our Accomplishments

A testament to our technical rigorousness, teamwork, and commitment to pioneering space technology in India.

CAN-7USAT INDIA 2025

National 2nd Place Winners

Secured the runner-up position in the national finals of the prestigious student space competition organized by the Indian National Space Promotion and Authorization Centre (IN-SPACe), competing against India's top engineering institutions.

98.4% Telemetry Accuracy
0.8m Landing Precision
0m Launch Altitude
0kg Satellite Mass
0Hz Data Transmission Rate
The Engineers

Meet Team Vayusat

A multidisciplinary team of engineering undergraduates from Dayananda Sagar University collaborating to conquer aerospace challenges.

Project Mentor
Dr. Prashantha Kumar

Dr. Prashantha Kumar

Faculty Adviser

Department of Aerospace Engineering, DSU

Charan Raj

Charan Raj

Project Lead

Systems Integration & Project Management

Keertan

Keertan

Electronics

Circuit Design & Sensor Integration

Saatvik

Saatvik

Electronics

PCB Design & Component Testing

Pragati

Pragati

Structures

Power Systems & Data Acquisition

Diya

Diya

Structures

Mechanical Design & Assembly

Manya

Manya

Structures

Structural Analysis & Recovery Systems

Shylesh

Shylesh

COMMs & Ground Station

Telemetry & RF Communication

Kelvin

Kelvin

COMMs & Ground Station

Ground Station Setup & Data Reception

MISSION IN ACTION
Team Vayusat with Luna MK-III Rocket on Launch Rail
Mission Chronicles

Our Past Year Journey

A visual archive of Team Vayusat's key design, assembly, electronics testing, and on-field model rocketry accomplishments.

Vayusat CanSat Avionics Assembly
Avionics Assembly
DSU Laboratory Team Display
Aerospace Rocket Model
Team Discussion in Aerospace Lab
Faculty Consultation
Parachute Recovery Preparation
Parachute Preparation
IN-SPACe National Competition Field
IN-SPACe National Finals
Model Rocket Nosecone Approval Seal
Nosecone Inspection
Team Selfie with Digital Twin Rocket Model
Team Selfie
Rocket Assembly and Fin Adjustments
Fin Calibration
Team Vayusat at the Launch Hangar
Hangar Posing
Solid Propulsion Model Rocket Display
DSU Rocket Showcase
DSU Rocket Standing on Thrust Tech India Launch Pad
On-Rail Launch Pad
Team Vayusat Receiving Competition Award
Award Ceremony
Team Vayusat posing with Luna MK-III Rocket
Luna MK-III Prep
National Model Rocketry Exhibition Stand
Rocket Exhibition
Vayusat Team and Dignitaries at the Exhibition
Exhibition Gathering
Ground Station Telemetry & Launch Feeds Monitoring
Live Launch Monitoring
CanSat Design Presentation to Jury Panel
Jury Evaluation
Recovery System Integration & Canopy Lines
CanSat Recovery System
Luna MK-III Avionics Bay Inspection
Payload Wire Audit
IN-SPACe CanSat India Trophy Close-up
National Trophy Close-up
Red 7U CanSat Model with Landing Legs
Deployable Landing Legs
Team Vayusat Stage Celebration with Trophy
Stage Celebration
Base Camp

Get In Touch

Interested in our aerospace research, sponsorship opportunities, or technical details? We would love to collaborate with you.

Institution

Dayananda Sagar University

Email Contact

eng23as0002@dsu.edu.in

Location

DSU Main Campus, Bengaluru, Karnataka, India

COMMs System Active