John Company

Department of the Air Force Report, 1996

DOW-UAP-D048 · page 5 of 181

Page 5 of 181 of DOW-UAP-D048

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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
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