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DOW-UAP-D48, Department of the Air Force Report, 1996
Page 3
3 / 181
Form Approved
REPORT DOCUMENTATION PAGE
0MB No. 0704-0188
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Davis Highway, Suite 1204, Arlington, VA 12202-4302, and to the Office of Management and Budget. Paperwork Reduction Project(0704-0188), Washington. DC 20503.
1. AGENCY USE ONLY (Leave blank) ~.• REPORT DATE
1
3. REPORT TYPE AND DATES COVERED
.
eptember 10, 1996
Final
4. TITLE AND SUBTITLE
5. FUNDING NUMBERS
f.1odeling Unlikely Space-Booster Failures in Risk Galculations
C: F04703-91-C-o112
TA:10/95-TT
6. AUTHORW
•
James A.
ard, Jr.
Robert M. Montgomery
7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES)
8. PERFORMING ORGANIZATION
REPORT NUMBER
Research Triangle Institute *
ACTA, Inc. **
RTl/5180m-43F
3000 N. Atlantic Avenue
· Skypark3
11
Cocoa Beach, FL 32931
23430 Hawthorne Blvd., Suite 300
Torrance, CA 90505
9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES)
10. SPONSORING/ MONITORING
AGENCY REPORT NUMBER
Department of the Air Force (AFSPC)
Department of the Air Force (AFSPC)
30th Space Wing
45th Space Wing
r\~'1~.1
-
-m.-t1<a-a
-
Vandenberg AFB, CA 93437
Patrick AFB, FL 32925
-Mr. Martin Kinna (30 SW/SEY)
Louis J. Ullian, Jr. (45 SW/SED)
11. SUPPLEMENTARY NOTES
*Subcontractor
" Prime Contractor
12a. DISTRIBUTION/AVAILABILITY STATEMENT
12b. DISTRIBUTION CODE
Distribution authorized to US Government agencies and their contractors to protect
administrative/operational use data; 10 September 96. Other requests for this document shall
be referred to the 30th Space Wing (AFSPC) Safety Office (30 SW/SE),Vandenberg AFB, CA
93437, or 45th Space Wing (AFSPC) Safety Office (45 SW/SE), Patrick AFB, FL 32925.
(!__,
13. ABSTRACT (Maximum 200 words)
Missile and space-vehicle performance histories contain many examples of failures that cause, or have the
potential to cause, significant vehicle deviations from the intended flight line. In RTl's risk-analysis program,
DAMP, such failures are referred to as Mode-5 failure responses. Although Mode--5 failure responses are much
less likely to occur than those that result in impacts near the flight line, risk-analysis studies are incomplete without
them. This report shows how Impacts from Mode-6 failures are modeled in program DAMP. The impact density
function used for this purpose contains two shaping constants that control the rate at which the density function
drops In value as the angular deviation from the flight line and the impact range increase. Certain Mode--5
•malfunctions are simulated, and the two shaping constants then chosen by trial and error so that impacts from the
simulated malfunctions and the theoretical density function are in close agreement. An appendix to the report
contains alisting and brief narrative failure history of the A~as, Delta, and Titan missile and space-vehicle launches
from the Eastern and Western Ranges from the beginning of each program through August 1996. Each entry
gives the vehicle configuration, whether the flight was asuccess, the flight phase in which any anomalous behavior
occurred, and aclassification of vehicl~ behavior in accordance with defined failure-response modes.
14. SUBJECT TERMS
15. NUMBER OF PAGES·
launch risk, unlikely failure modeling, booster failure probabilities
180
16. PRICE CODE
17. SECURITY CLASSIFICATION
18. SECURITY CLASSIFICATION
19. SECURITY CLASSIFICATION
20. LIMITATION OF ABSTRACT
OF REPORT
OF THIS PAGE
OF ABSTRACT
Unclassified
lJnclassified
lnclasslfled
SAR
NSN 7540-01-280-5500
Standard Form 298 (Rev. 2-89)
Prescribed by AIIISI Std. Z39-18
298·102
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