CAVU Aerospace UK

Lowering the Barrier to Space Imaging for CubeSat and SmallSat Operators

Access to high-performance Earth observation imagery should not be limited by long lead times, high NRE costs, or payload development risk. At Cavu Aerospace, we have developed a practical and scalable camera strategy specifically tailored for CubeSats and small satellites — enabling faster development cycles and significantly lower upfront costs.

Space Imaging, CubeSat, SmallSat, Earth observation imagery, camera, small satellites

The Challenge in Small Satellite Imaging

Small satellite missions — particularly in the CubeSat class such as CubeSat platforms — operate under strict SWaP (Size, Weight, and Power) constraints. At the same time, customers expect increasingly higher image resolution and reliability.

Traditionally, optical payload development involves:

  • Long lead times for bespoke lens assemblies
  • High engineering model (EM) costs
  • Limited early access to flight-representative electronics
  • Delays in ADCS and OBC functional testing

This slows down mission validation and increases program risk.

Our Two-Stage Camera Delivery Model

We have introduced a dual-phase strategy that separates electronic payload validation from final optical optimization, without compromising flight heritage.

       1. Engineering Model (EM) — Immediate, Affordable, Functional

For Engineering Models, we provide:

  • Flight-representative electronics
  • Identical sensor, processing, and interface architecture as Flight Model (FM)
  • Commercial off-the-shelf (COTS) optical assemblies
  • Immediate shipment capability
  • Significantly reduced cost

This enables customers to:

  • Perform early ADCS testing
  • Validate image pipeline and compression
  • Test data handling with their onboard computer
  • Conduct environmental and integration tests
  • Run functional system validation months earlier

Critically, the electronics architecture remains unchanged between EM and FM, reducing downstream redesign risk.

       2. Flight Model (FM) — Bespoke Optical Assembly

For the Flight Model, we introduce:

  • Custom-designed, mission-optimized lens assemblies
  • GSD optimization based on orbit altitude
  • Mechanical and thermal space-qualified integration
  • Radiation-considered component selection

This ensures performance alignment with final mission requirements while preserving the validated electronic architecture.

Space Imaging, CubeSat, SmallSat, Earth observation imagery, camera, small satellites

Scalable Camera Platforms: 2U, 3U & 12U

We support multiple form factors aligned with industry standards:

  • 2U payload configuration 1.4 kg FM, 18 cm optic assembly, 400mm focal length
  • 3U payload configuration, 26 cm optic assembly, 200mm focal length
  • 12U high-performance configuration, 26 cm optic assembly, 200mm focal length

These configurations integrate seamlessly into standard CubeSat buses and small satellite platforms.

 

Sensor Options: From Technology Demo to Commercial EO

We offer three sensor classes:

5 MP

Ideal for:

  • Technology demonstrators
  • Earth context imaging
  • Educational missions
  • Constellation experiments

16 MP

The commercial sweet spot for:

  • Agricultural monitoring
  • Environmental analysis
  • Maritime domain awareness
  • Mid-resolution Earth observation

51 MP

Designed for:

  • Higher-performance small satellites
  • Detailed mapping missions
  • Commercial Earth observation constellations

Enhanced spatial analytics

camera, image, image sensor, satellite, satellite systems, Space Imaging, CubeSat, SmallSat, Earth observation imagery, camera, small satellites

Ground Sample Distance (GSD)

Depending on orbit altitude and optical configuration, our systems deliver:

1.5 m to 10 m Ground Sample Distance

Image sensors have 3.4 Mico meter pixel size. This range supports:

  • Broad-area monitoring (10 m class)
  • Commercial-grade observation (~3–5 m)
  • High-resolution small-satellite imaging (~1.5 m class)

Importantly, GSD is achieved through optical optimization — not megapixel marketing — ensuring physics-driven performance.

 

Why This Model Matters

Small satellite programs — particularly in the NewSpace sector — require:

  • Rapid iteration cycles
  • Lower capital exposure during early development
  • Reduced procurement risk
  • Clear migration path from EM to FM

Our approach enables:

✔ Early system validation
✔ Lower non-recurring engineering cost
✔ Reduced integration risk
✔ Faster time to launch
✔ Scalable performance across mission classes

 

Built for the New Space Economy

Companies such as Planet Labs and emerging EO operators have demonstrated the power of constellation-based imaging. However, entry barriers remain high for startups, research missions, and institutional programs.

Our affordable EM strategy lowers that barrier.

By providing immediate-access engineering models paired with mission-optimized flight optics, we bridge the gap between laboratory validation and orbit-ready performance.