Department of the Air Force Report, 1996

U.S. Department of War · 1996-09-10 · 181 pages · text from the file's own layer

This final report, dated September 10, 1996, was prepared by the Research Triangle Institute for the Department of the Air Force's 45th and 30th Space Wing safety offices. Titled Modeling Unlikely Space-Booster Failures in Risk Calculations, it shows how rare Mode-5 failures, in which a rocket veers well off its intended flight line, are modeled in the DAMP risk-analysis program. An appendix lists Atlas, Delta, Titan and Thor launch and failure histories through August 1996.

From the source:Release of 2026-05-08 Incident: 9/10/96, N/A. This report describes the Modeling of Unlikely Space-Booster Failures in Risk Calculations, documenting historical launch failure modes and recommending corrective actions to address them using novel modelling techniques.

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“Titan II”13 pages

p. 5 …64 6.4 Shaping Constants for Titan IV................................................................................ 65 6.5 Shaping Constants for LLVl .................................................................................... 69…
p. 74 …6.4 Shaping Constants for Titan IV Mode-5 shaping constants for Titan IV were developed…
p. 77 …Shaping Constants for Titan IV TB (sec) Breakupqa (deg-lb/ft2) B A II 300 none…
p. 109 …Titan IIIC and later configurations to include IIIB, IIID, IIIE, 34B, 34D, III/CT, IV, II…
p. 155 …Titan II SLV was developed from refurbished Titan II ICBMs incorporating technology and hardware from the…
p. 156 …Summa of Titan Vehicle Confi rations Descri Titan II ICBM converted to a man-rated vehicle…
p. 159 …2 0 54 WS (first Titan II) 03/16/62 II (N-2) ER 0 55…
p. 160 …08/13/64 II (8-7) WR 0 104 SV (first Titan Ill) 09/01/64…
p. 166 D.4.2 Titan Failure Narratives The following narratives provide available details about each Titan failure…
p. 168 …Stage II engine shut down prematurely due to oxidizer bootstrap-line failure. 76. Titan I (Mares…
p. 169 …Titan II (Thread Needle), 20 June 63, Response Mode 5, Flight Phase 2: Flight appeared normal…
p. 170 …Titan II (Bold Guy), 21 Sep 65, Response Mode 4, Flight Phase 2: After a normal…
p. 172 …Following a successful Titan-II second-stage burn and after payload separation, the apogee- kick motor…

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No. Mission/ID
Launch
Date
Vehicle
Confiauration
Test
Ranae
Response
Mode
Flight
Phase
Rep.
Conf.
IMP-C 05/29/65 DSV-3C ER 0
TIROSOT-1 07/01/65 DSV-3C ER 0
OSO-C 08/25/65 DSV-3C ER 4 2.5 0
GEOSA
PIONEER A
TIROSOT-3
TIROSOT-2
11/06/65
12/16/65
02/03/66
02/28/66
DSV-3E
DSV-3E
DSV-3C
DSV-3E
ER
ER
ER
ER
NA 2&5 0
0
0
0
AE-8
AIMP-0
05/25/66
07/01/66
DSV-3C
DSV-3E
ER
ER
NA
NA
2&5
2.5&5
0
0
PIONEER-8 08/17/66 DSV-3E ER 0
TOS 10/02/66 DSV-3E WR 0
lNTELSAT 11 (F-1)
BIOS-A
INTELSAT II (F-2)
TOS
10/26/66
12/14/66
01/11/67
01/26/67
DSV-3E
DSV-3G
DSV-3E
DSV-3E
ER
ER
ER
WR
0
0
0
0
OSO-E1 03/08/67 DSV-3C • ER 0
INTELSAT II (F-3) 03/22/67 DSV-3E ER 0
TOSO 04/20/67 DSV-3E WR 0
IMP-F 05/24/67 DSV-3E WR 0
AIMP-E
8108-8
INTELSAT II (F-4)
07/19/67
09/07/67
09/27/67
DSV-3E
DSV-3G
DSV-3E
ER
ER
ER
0
0
0
OS0-D 10/18/67 DSV-3C ER 0
TOS-C
PIONEER-C
11/10/67
12/13/67
DSV-3E
DSV-3E
WR
ER
0
0
GEOS-8
RAE-A
TOS-E
INTELSAT Ill-A
PIONEER-0
01/11/68
07/04/68
08/16/68
09/18/68
11/08/68
DSV-3E
DSV-3E
DSV-3L
DSV-3L
DSV-3E
WR
WR
WR
ER
ER
5 1
0
0
0
0
0
HEOS-A 12/05/68 DSV-3E ER 0
TOS-F
INTELSAT 111-C
O80-F
ISIS-A
INTELSAT 111-B
TOS-G
12/15/68
12/18/68
01/22/69
01/30/69
02/05/69
02/26/69
DSV-3L
DSV-3L
DSV-3C
DSV-3E
DSV-3L
DSV-3E
WR
ER
ER
WR
ER
ER
0
0
0
0
0
0
INTELSAT 111-D 05/21/69 DSV-3L ER 0
IMP-G
BIOS-D
INTELSAT 111-E
OS0-G
PIONEER-E
IDCSP/A-A
INTELSAT 111-F
TIROs-M
06/21/69
06/29/69
07/26/69
08/09/69
08/27/69
11/22/69
01/14/70
01/23/70
DSV-3E
DSV-3L
DSV-3L
DSV-3L
DSV-3L
DSV-3L
DSV-3L
DSV-3L
WR
ER
ER
ER
ER
ER
ER
WR
5
5
3&5
1
0
0
0
0
0
0
0
0
9/10/96 137 RTI

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Report, from the pursue collection. The PDF is mirrored here; the original link is above. 181 pages are in the text index: search them above, or from the library's search.