Inactive
Notice ID:NASA-GSFC-POD-ESE1-Limb-Viewing-Concept-SC
Amendment 6 - The purpose of this amendment is to change the response date from April 15, 2022 to April 22, 2022 at 5 PM EDT. Further Part 1 and Part 2 of the POD documentation has been updated. Chang...
Amendment 6 - The purpose of this amendment is to change the response date from April 15, 2022 to April 22, 2022 at 5 PM EDT. Further Part 1 and Part 2 of the POD documentation has been updated. Changes to the POD documentation are noted with yellow highlights and/or red strikethroughs. These documents are included in the "Attachments/Links" section of this posting. Amendment 5 - The purpose of this amendment is to incorporate the revised Questions & Answers document "2022 0412 Limb-Viewing ESE Mission POD QA Rev1" as an attachment. Amendment 4 - The purpose of this amendment is to incorporate the Questions & Answers document "2022 0412 Limb-Viewing ESE Mission POD QA" as an attachment. Amendment 3 - The purpose of this amendment is to change the response date from April 15, 2022 to April 22, 2022 at 5 PM EDT. Amendment 2 - The purpose of this amendment is to change the response date from April 11, 2022 to April 15, 2022 at 5 PM EDT. Amendment 1 - The purpose of this amendment is to update the POC for questions and submissions from Julie Breed to Caleb M. Principe at Caleb.M.Principe@nasa.gov. All references to Julie Breed in the initial posting should be considered replaced as a result of this amendment. This partnership opportunity is being issued to select teaming partner(s) to serve as the satellite integrator for an individual mission; provide flight-qualified Class C spacecraft bus (our mission is not compatible with a CubeSat platform), instrument to spacecraft integration support, environmental testing, integration support for the spacecraft to launch vehicle, and initial mission operations (launch and early orbit operations). GSFC intends to maintain an essential degree of insight into satellite integration and will exercise essential oversight to ensure that the implementation is responsive to NASA requirements and constraints as will be defined in upcoming AO. See Attached.
