AERODYNAMIC PERFORMANCE ANALYSIS SLV-3/AGENA/LUNAR ORBITER,
Abstract
The open-loop design reference trajectory data used to analyze the capability of the SLV-3 to perform its role for the Lunar Orbiter (LO) mission are presented. This information is required by the various design groups for computation of aerodynamic heating and of structural, dynamic, and aerodynamic loads. The principal trajectory design data presented include: mission profile and SLV-3 mission requirements; launch vehicle description; aerodynamics, propulsion, weights, and environmental data; Trajectory design constraints; and exchange coefficients.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 21, 1966
- Accession Number
- AD0480572
Entities
People
- D. F. Meacock
Organizations
- General Dynamics