For missions with low tip-off requirements, switches may be required on either the payload or launch vehicle. Mounting details will be specified in the ICD. 8.0 Payload Environment The Contractor shall provide data for the maximum payload acoustic, vibration, shock, and acceleration, and thermal environment levels during launch and ascent. The maximum electromagnetic radiation levels encountered by the payload shall be depicted in Figure D1-3. The Contractor shall illustrate the pressure profiles and depressurization rates for each PLF in Figure D1-4. The maximum expected payload flight environments due to acoustics (50% fill), vibration, and shock shall be shown in Tables D1-K, D1-L, and D1-M, respectively. The maximum expected total acceleration (limit load factors), including uncertainty factors, shall be shown in Table D1-N (key dynamic events may be broken out as appropriate). The maximum expected sinusoidal vibrations at the base of the PA shall be shown in Table D1-O. The maximum quasi-steady acceleration as a function of payload separated mass shall be shown in Figure D1-5. The Contractor shall provide the maximum thermal environment during ascent for every launch component (i.e., upper stage, unblanketed skin, thermal/acoustic blankets, etc.) inside the fairing with a view factor to the payload in Figure D1-5A. TBP Figure D1-3: Maximum Electromagnetic Radiation Levels Encountered on Payload TBP Figure D1-4: PLF Pressure Profiles and Depressurization Rates TBP
For missions with low tip-off requirements, switches may be required on either the payload or launch vehicle. Mounting details will be specified in the ICD. 8.0 Payload Environment The Contractor shall provide data for the maximum payload acoustic, vibration, shock, and acceleration, and thermal environment levels during launch and ascent. The maximum electromagnetic radiation levels encountered by the payload shall be depicted in Figure D1-3. The Contractor shall illustrate the pressure profiles and depressurization rates for each PLF in Figure D1-4. The maximum expected payload flight environments due to acoustics (50% fill), vibration, and shock shall be shown in Tables D1-K, D1-L, and D1-M, respectively. The maximum expected total acceleration (limit load factors), including uncertainty factors, shall be shown in Table D1-N (key dynamic events may be broken out as appropriate). The maximum expected sinusoidal vibrations at the base of the PA shall be shown in Table D1-O. The maximum quasi-steady acceleration as a function of payload separated mass shall be shown in Figure D1-5. The Contractor shall provide the maximum thermal environment during ascent for every launch component (i.e., upper stage, unblanketed skin, thermal/acoustic blankets, etc.) inside the fairing with a view factor to the payload in Figure D1-5A. TBP Figure D1-3: Maximum Electromagnetic Radiation Levels Encountered on Payload TBP Figure D1-4: PLF Pressure Profiles and Depressurization Rates TBP
146413-SOL-001-003.docx