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Aerospace Engineering Commons

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Full-Text Articles in Aerospace Engineering

Enzothrust Testo Booster, Wanxmkkfsfrs Wanxmkkfsfrs Sep 1995

Enzothrust Testo Booster, Wanxmkkfsfrs Wanxmkkfsfrs

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Simulation Of Temperature Variation In Parachute Inflation, D. K. Chaturvedi Sep 1995

Simulation Of Temperature Variation In Parachute Inflation, D. K. Chaturvedi

D. K. Chaturvedi Dr.

In this paper, the variation of temperature during parachute inflation is simulated by system dynamics methodology. In this methodology, causal loops for system have been identified and flow diagram is drawn. Flow diagram consists of flow rate variables, level variables and auxiliary variables. In causal mechanism principal feedback loops are identified. It also simplfies illustration due to various influencing factors such as pressure, rate of pressure, mass of parachute, textile characteristics, motion of folded parachute to compresion under pressure and interaction between parachute and its container/bag.


A Unified Topological Approach To Electromagnetic Environmental Effects Protection, George H. Baker, J. Philip Castillo, Edward F. Vance Jun 1995

A Unified Topological Approach To Electromagnetic Environmental Effects Protection, George H. Baker, J. Philip Castillo, Edward F. Vance

George H Baker

The presentation recommends an approach for unifying electronic system protection designs for a wide spectrum of electromagnetic environments. A general electromagnetic topological construct is developed as the basis for a consistent shielding and terminal protection methodology. Spectral characteristics of multiple interfering electromagnetic sources, both internal and external, are described. Effects addressed include EMI/EMC, lightning, nuclear EMP, and RF weapons. Protection practices for individual effects are discussed and means for integrating these into a single protection topology.