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<b>Nile-View 1: Advancing Earth Observation in Egypt via Cost-Efficient CubeSats</b>

Domaine:

geospatialenvironment and energy

Type de record:

project
Créateur:
Sed
Éditeur:
fig
Hôte:avatar
Nile-View 1 is a 3U CubeSat platform designed in alignment with the national development priorities of Egypt, optimized for low-cost, high-value Earth observation data. The mission bridges the gap between commercial off-the-shelf (COTS) small satellite technology and precision environmental intelligence, establishing an end-to-end operational framework. Objectives:1. Environmental Monitoring: Continuous tracking of water levels, flood extents, and vegetation health across the Nile River basin to support agricultural planning. 2. Infrastructure Tracking: Systematic monitoring of urban expansion and construction progress in the New Administrative Capital to enable evidence-based urban planning. 3. Capacity Building: Hands-on framework for satellite integration, ground operations, and mission control. Technical Specifications & Architecture:• Orbital Mechanics: 500 km Sun-Synchronous Orbit (SSO) with a 97.4° retrograde near-polar inclination, delivering a 48-hour revisit cycle over Egypt under consistent solar illumination. • Engineering Payload: High-resolution multispectral imager capturing Visible (RGB) and Near-Infrared (NIR) bands, achieving a 4.5-meter spatial resolution optimized for NDVI (Normalized Difference Vegetation Index) mapping. • Electrical Power System (EPS): Dual deployable solar arrays with triple-junction photovoltaic cells paired with a 45 Wh Lithium Iron Phosphate (LFP) battery assembly, supporting an 18W peak power demand during simultaneous imaging and downlink phases. • Communications: Dual-link architecture utilizing a bi-directional UHF/VHF link for command/telemetry (spacecraft health monitoring) and a high-rate 5 Mbps S-Band link for transferring multispectral science data directly to the ground station network in Cairo. The total spacecraft wet mass is capped at 4.2 kg, fitting strictly within 3U launch constraints. Leveraging space-grade COTS components and a commercial rideshare launch model, the entire program budget is structured at an incredibly cost-efficient $150,000, serving as a scalable model for future indigenous space programs.

Visit

doi.org

Tags

Aerospace engineering not elsewhere classifiedPhotogrammetry and remote sensingSatellite communicationsSatellite-based positioningEnvironmental management

Licenses

Creative Commons Attribution 4.0 Internationalhttps://creativecommons.org/licenses/by/4.0/legalcode

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