Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19660009179

Atlas-Centaur ac-5 analog/digital load reduction autopilot study

View original source ↗Export metadata ↓

Abstract

Analog digital evaluation of load reduction autopilot on Atlas Centaur AC-5 vehicle

Explore related subjects

LOAD FACTOR DIGITAL TECHNIQUE AUTOPILOT BENDING MOMENT ATLAS CENTAUR LAUNCH VEHICLE

Keep this discovery

Explore connections, maps & timelines

Harris, R.. 1964-02-13. Atlas-Centaur ac-5 analog/digital load reduction autopilot study. https://ntrs.nasa.gov/citations/19660009179

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1967

Aeroelastic load growth effects on Saturn configurations

Analytical evaluation of aerodynamic load growth or steady state aeroelastic effect for Saturn configurations

LOAD FACTOR↗

NASA NTRS1965

The reliability of the electric contact

Dependence of electric contact reliability on operating conditions of circuit and load parameters

LOAD FACTOR↗

NASA NTRS1964

Study for the indicial load effects on multistage space vehicle systems. volume iii- a description of the computer programs employed annual summary report, 21 jun. 1963 - 20 aug. 1964

Documentation of computer programs used to study load effects on multistage space vehicle systems

LOAD FACTOR↗