Centaur Interim Upper Stage (IUS) System Study. Volume 1. Executive Summary
Abstract
The overall objective of this system study was to provide preliminary design(s), airborne and ground interface definition, substantiated life-cycle cost estimates and total program definitions for a Centaur Interim Upper Stage (IUS) System. The IUS system consists of a primary propulsive stage (a Centaur version), auxiliary propulsive stage(s) (when required), airborne support equipment, aerospace ground equipment, software, and unique facilities. Six alternative Centaur IUS programs were defined; each satisfying DOD and/or NASA requirements as specified in SAMSO document SR-IUS-100, 'Interim Upper Stage (IUS) System Requirements', Change 3, dated 4 April 1975. The IUS programs defined in the study incorporate a primary propulsive stage based on the existing D-1 Centaur vehicle used by NASA for Viking and by DOD for FleetSatComm.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 31, 1975
- Accession Number
- ADA021401
Entities
People
- A. W. Nelson
- C. F. Peters
- D. A. Heald
- R. D. Harris
Organizations
- General Dynamics