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Innovation - Cubsat Mission

Innovation › Innovation - Cubsat Mission

PROJECT SBB-1:MISSION DASHBOARD

Validating “First Principles” in Low Earth Orbit.

Mission Profile

Project SBB-1 is not a simulation. It is a fully functional CubeSat designed, built, and tested by students under the mentorship of aerospace professionals. The payload was fully flight-qualified and integrated for Low Earth Orbit operations, while validating core educational methodology. This mission represents the culmination of rigorous engineering, academic discipline, and real-world space systems experience.

MISSION TYPE
Technology Demonstration
ORBIT
Low Earth Orbit (LEO)
PRIMARY GOAL
Validate “First Principles” Learning
SECONDARY GOAL
On-Orbit Sensor Data Acquisition
DOI
10.5281/zenodo.18195108
SYSTEM ARCHITECTURE

System Overview

Onboard Compute Unit
The Brain
Custom-designed flight computer managing all satellite operations, fault processes, and autonomous decision-making.
  • ARM Cortex-M7 Core
  • Fault-tolerant logic
  • Real-time OS
Payload Systems
The Senses
Integrated sensor suite capturing environmental data across multiple parameters for in-orbit validation.
  • 9-DOF IMU array
  • Thermal monitoring
  • Environmental sensors
Telemetry & Comm
The Voice
UHF/VHF communication system enabling reliable ground station contact and beacon transmissions.
  • UHF downlink
  • VHF uplink
  • Packet & sync
MISSION COMPLIANCE

Institutional Framework & Compliance

A mission is only as credible as the institutions that authorize and support it. SBB-1 is embedded within a rigorous regulatory and mentorship ecosystem.

Authorized by
IN-SPACE
Project SBB-1 operates under official authorization from IN-SPACe.
Mentored by
Industry
Guidance provided by aerospace partners, ensuring flight-ready standards.
Data
Integrity
Mission data is processed, validated, and archived for research-grade outputs.
Lab
SYSTEM ARCHITECTURE

System Overview

System overview
Media
01
Conceptualization

Mission definition, feasibility studies, and initial system architecture design.

02
Prototyping

Breadboard models, component selection, and early integration testing.

03
Engineering Model

Full-scale functional prototype with flight representative components.

04
Qualification

Vibration, thermal vacuum, and EMC testing to space-grade standards.

05
Launch Integration

Final assembly, pre-flight checkout, and integration with PSLV.

06
Mission Conclusion

Payload successfully integrated. Mission concluded due to launch vehicle anomaly (Jan 12, 2026).

We didn't just teach them about space. We gave them a ticket to go there.

Campus building
Nobel Peace Center
UNESCO
AMI
US Department of State
Seal
Nobel Peace Center
UNESCO
AMI
Nobel Peace Center
UNESCO
AMI
US Department of State
Seal
Nobel Peace Center
UNESCO
AMI