Appendix_C.pdf
PDF 915 KB Posted
- Attached to
- Titan IV Crane Lift
- Solicitation number
- FA8601-16-T-0063
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SOW Appendix C
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Other files
| File | Type | Posted |
|---|---|---|
| Amendment_2_Synopsitation_Titan_IV_Crane_Lift.docx | DOCX document | |
| Amendment_1_Synopsitation_Titan_IV_Crane_Lift.docx | DOCX document | |
| Appendix_B.pdf | ||
| DFARs_252_209-7991.pdf | ||
| Synopsitation_Titan_IV_Crane_Lift.docx | DOCX document | |
| FA8601-16-T-0063.doc | DOC document | |
| DD_Form_1423_-_CDRL_A0001_Exhibit_1_(2).pdf | ||
| Wage_Determination_2005-2419_8_Jul_15.pdf | ||
| Titan_IV_Move_SOW_4_Dec_15.docx | DOCX document | |
| Appendix_A.pdf |
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Text version
1. wide shot balls
3. left side socket
2. wide shot sockets
4. right side socket
Appendix C. Photos of Ball and Socket Joint
Weights and Measurements:
Solid Rocket Motor Upgrade (SRMU):
There are two (2) SRMUs
10.5 feet in diameter, 112 feet long, approximately 75,000 pounds.
Stage One Core Vehicle:
• Stage One Core Vehicle that is 10 feet in diameter, 86.5 feet long, approximately 18,000 pounds.
File details come from the government source that posted it. Updated .