Integrated Bus/Instrument Performance Effects. The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements: 3.2.1.6.1.1 [**Redacted**] [**Redacted**] 3.2.1.6.1.2 [**Redacted**] [**Redacted**]
Appears in 2 contracts
Samples: Worldview 3 Satellite Purchase Agreement (Digitalglobe Inc), Satellite Purchase Agreement (Digitalglobe Inc)
Integrated Bus/Instrument Performance Effects. The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements:
3.2.1.6.1.1 [**Redacted**] [**Redacted**]
3.2.1.6.1.2 [**Redacted**] [**Redacted**]
Appears in 2 contracts
Samples: Worldview 3 Satellite Purchase Agreement (Digitalglobe Inc), Worldview 3 Satellite Purchase Agreement (Digitalglobe Inc)
Integrated Bus/Instrument Performance Effects. The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements:
3.2.1.6.1.1 [**Redacted**] [**Redacted**]
3.2.1.6.1.2 [**Redacted**] [**Redacted**]
Appears in 2 contracts
Samples: Worldview3 Satellite Purchase Agreement (Digitalglobe, Inc.), Worldview 3 Satellite Purchase Agreement (Digitalglobe Inc)
Integrated Bus/Instrument Performance Effects. The SSI shall perform appropriate integrated Satellite-level analyses and design work in order to ensure the Satellite meets the following performance requirements. LOS motion shall be calculated using an Instrument Finite Element Model (FEM) provided by the Instrument Contractor as defined under Applicable Documents, which shall be assumed to meet the following requirements:
3.2.1.6.1.1 [**Redacted**] [**Redacted**]
3.2.1.6.1.2 [**Redacted**] [**Redacted**]: ITAR-Controlled Document DigitalGlobe Proprietary and Confidential Use or disclosure of data is subject to the restriction on the title page of this document.
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