Labels:text | font | screenshot | black and white | document OCR: NSTS 17462-50 Revision H c. UVPI will receive state vectors real time. 4.2 Space Shuttle Placards/Constraints/Limitations The following are constraints on this flight that are more restrictive than the baseline design. This does not necessarily reflect all constraints, limitations, or placards on the Space Shuttle at this time but are those of primary concern to this flight. Reference should also be made to the Shuttle Operational Data Book Volume I, JSC 08934, for standard placards and constraints. a. None identified 5.0 SUPPLEMENTAL REQUIREMENTS 5.1 Development Test Objectives The following Development Test Objectives (DTO's) are assigned to this flight: DTO 0236 Ascent Aerodynamic Distributed Loads Verification on OV-102 (Higher than nominal angle of attack) # DTO 0251 Entry Aerodynamic ...
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