Department of the Air Force Report, 1996
DOW-UAP-D048 · page 5 of 181
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Table of Contents · 1. Introduction............................................................................................................................... 1 2. Examples Showing Need for Mode 5 ................................................................................ 3 3. Understanding the Mode-5 Failure Response ................................................................... 7 3.1 Effects of Mode-5 Shaping Consta.nts ................................. " ..................................... -...... 9 3.2 Effects of Shaping Constant on DAMP Results ........................................................ 9 4. Methodology for Assessing Failure Probabilities ........................................................... 13 4.1 The Parts-Analysis Approach .................................................................................. 13' 4.2 The Empirical Approach .......................................................................................... 15 5. Computation of Failure Probabilities ............................................................................... 16 5.1 Overall Failure Probability ....................................................................................... 16 5.2 Relative and Absolute Probabilities for Response Modes ..................................... 24 5.3 Relative Probability of Tumble for Response-Modes 3 and 4 ............................... 30 6. Shaping Constants Through Simulation .......................................................................... 31 6.1 Malfunction Tum. Simulations........... • ...................................................................... 31 6.1.1 Random-Attitu.de Failures ...............-............................................................... 31 6.1.2 Slow-Tum Failures ........................................................................................... 32 6.1.3 Factors Affecting Malfunction-Tum Results ................................................ 33 6.1.4 Malfunction-Tum Results for Atlas IIAS ...................................................... 35 6.2 Shaping Constants for Atlas IIAS ............................................................................ 37 6.2.1 Optimum Mode-5 Shaping Constants ........................................................... 37 6.2.2 Launch-Area Mode-5 Risks ............................................................................ 49 6.2.3 Effects of Mode-5 Constants on Ship-Hit Contours ..................................... 51 6.2.4 Range Distributions of Theoretical and Simulated Impacts ........................ 58 6.3 Shaping Constants for Delta-GEM .......................................................................... 60 6.3.1 Optimum Mode-5 Shaping Constants ........................................................... 61 6.3.2 Launch-Area Mode-5 Risks ............................................................................ 64 6.4 Shaping Constants for Titan IV................................................................................ 65 6.5 Shaping Constants for LLVl .................................................................................... 69 6.6 Shaping Constants for Other Launch Vehicles ....................................................... 72 7. Potential Future Investigations ......................................................................................... 73 8. Summarv: ., ............................................................................................................................ 74 9/10/96 ii RTI I