A Design Method of L/D Control Program for Atmospheric Re-Entry
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概要
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It is required for a vehicle to control lift to drag ratio (L/D) during atmospheric re-entry to keep aerodynamic heat-rate or axial load factor at constant level. The L/D programs under such constraints are analytically solved directly from the equations of motion. A transfer flight mode to connect the constant heat-rate mode and constant axial load mode is introduced and also solved.
- 特定非営利活動法人 日本ロケット協会の論文
特定非営利活動法人 日本ロケット協会 | 論文
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