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Space systems -- Unmanned spacecraft -- Estimating the mass of remaining usable propellant by Windows XP Mode is a reference work available to read on EtoBox.
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1 Scope 5 2 Normative references 5 3 Terms and definitions 5 4 Objectives 6 4.1 General 6 4.2 Objectives in estimating mass of remaining usable propellant 6 5 Requirements 6 5.1 Selection of estimation method 6 5.2 Estimation of propellant mass 6 5.3 Uncertainty of estimation 7 5.4 Incorporating required function into spacecraft design 7 5.5 Documentation of data 7
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- Windows XP Mode
- Language
- EN
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- reference
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