Accession Number:

AD0843344

Title:

Trajectory Design for Centaur Missions,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Snyder, R. E.

Report Date:

1961-07-06

Pagination or Media Count:

16.0

Abstract:

The report describes a program for efficiently designing trajectories for the Centaur first burn phase of flight. Author

Descriptors:

• *LAUNCH VEHICLES
• GUIDED MISSILE TRAJECTORIES
• COMPUTER PROGRAMMING
• AZIMUTH
• APOGEE
• PARTIAL DIFFERENTIAL EQUATIONS
• FLOW CHARTING
• MATHEMATICAL ANALYSIS
• BOOSTER ROCKET ENGINES

Subject Categories:

• Spacecraft Trajectories and Reentry
• Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE