Technical Blueprint · Rev A

Sustaino-1 1P PocketQube spacecraft.

Actively transitioning from 3D-printed tough-PLA test frames into carbon-fibre composite flight hardware for the Sustaino-1 airframe.

Spacecraft Bus

Physical & Compute Specification

Outer envelope
50 × 50 × 50 mm
Inner cavity
46 mm (2 mm uniform walls)
Integrated mass
0.245 kg
Processor
Raspberry Pi Pico 2 · RP2350 Dual-Core
Memory
520 KB SRAM · 4 MB Flash
Class
1P PocketQube
Payload Array

Instrument Manifest

  • P01
    GY-521 MPU-6050
    Orientation Gyro / IMU
  • P02
    OV7670 CMOS
    Visual Tracker Camera
  • P03
    AHT20 + BMP280
    Climate & Barometric Module
  • P04
    Nitinol SMA Loop
    Passive Antenna Deployment
  • P05
    5V Passive Beacon
    Audio Recovery Signal
Internal Packaging Stack

Base Power → 45° Brain Rail → Ceiling Payload

A three-layer volumetric strategy that maximises payload density inside the 46mm cavity while keeping thermal, power and RF paths cleanly segregated.

┌──────────────────────────────────────────┐
│  ▲ CEILING PAYLOAD INSETS                │
│    · OV7670 Visual CMOS Tracker          │
│    · Nitinol SMA Antenna Loop            │
│    · 5V Passive Audio Beacon             │
├──────────────────────────────────────────┤
│  ◆ 45° DIAGONAL FLOATING BRAIN RAIL      │
│    · Raspberry Pi Pico 2 (RP2350)        │
│    · GY-521 MPU-6050 IMU                 │
│    · AHT20 + BMP280 Climate              │
├──────────────────────────────────────────┤
│  ▼ BASE POWER LAYER                      │
│    · 3-Cell LiPo · Charge Controller     │
│    · Solar Harvest Bus · 5V Rail         │
└──────────────────────────────────────────┘
          46mm inner cavity · 2mm walls
Airframe Blueprint

50mm cube · exploded schematic

CEILING · Camera / Antenna45° Brain Rail · RP2350BASE · Power / LiPo50mm envelope46mm inner cavityEAK-ORBITALS · SUSTAINO-1 · REV ASCALE 4:1 · UNITS mm · ISO PROJECTIONMASS 0.245 kg