This Spacecraft Engineering eBook from 3D-LABS is written for engineers and students who want a clear, practical reference they can apply immediately.
Spacecraft Engineering — A Working Guide provides a systems engineering framework covering all bus subsystems (structure, thermal, power, ADCS, propulsion, C&DH) with mass, power, and thermal budget worksheets. Written for spacecraft systems engineers and subsystem leads.
What format and standards does this book follow?
Subsystem-budget-to-architecture structure per ECSS-E-ST-20C (electrical), ECSS-E-ST-31C (thermal control), ECSS-E-ST-60-10C (AOCS/GNC), and NASA-HDBK-1001 terrestrial environment criteria.
What spacecraft mass budget formula is used?
M_wet = M_dry + M_propellant, where M_propellant = M_dry*(exp(delta-v/(Isp*g0))-1). Dry mass contingency: 20% at Phase A/B, 10% at Phase C/D per ECSS. Structural mass fraction: 15-25% of dry mass for GEO commsats.
Is this book applicable to Indian spacecraft programmes?
Yes – ISRO GSAT-series and Resourcesat-2A heritage data, IN-SPACe compliance documentation requirements, and ISRO environmental test standards (vibration, thermal vacuum, EMC) are all referenced.
How do I access this book after purchase?
eBook PDF: Instant download via email and 3D-LABS dashboard. Paper Book: Printed and shipped to India.
What’s Included
An instant PDF download covering the core concepts, practical examples, and key references — ready to read on any device.
