Author: M. J. QueijoPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 72
Book Description
Fixed-base-simulator Study of the Ability of a Pilot to Perform Soft Lunar Landings
Author: M. J. QueijoPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 72
Book Description
Fixed-base-simulator Study of Ability of Pilots to Perform Soft Lunar Landings by Using a Simplified Guidance Technique
Author: G. Kimball MillerPublisher:
ISBN:
Category : Lunar landing sites
Languages : en
Pages : 34
Book Description
Fixed-base-simulator Study of the Ability of a Pilot to Perform Soft Lunar Landings
Author: M. J. QueijoA Fixed-base-simulator Study of the Ability of a Pilot to Establish Close Orbits Around the Moon and to Perform Soft Lunar Landings
Author: M. J. QueijoPublisher:
ISBN:
Category : Space flight to the moon
Languages : en
Pages : 8
Book Description
NASA Technical Note
Author: A Fixed-base-simulator Study of the Ability of a Pilot to Establish Close Orbits Around the Moon
Author: M. J. QueijoPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 58
Book Description
A Fixed-base-simulator Study of the Ability of a Pilot to Establish Close Orbits Around the Moon
Author: M. J. QueijoPublisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
A study was made on a six-degree-of-freedom fixed-base simulator of the ability of a human pilot to modify hyperbolic ballistic trajectories of a space vehicle approaching the moon so as to establish a circular orbit 50 miles above the lunar surface. The pilot was given control of thrust along the vehicle's longitudinal axis and torques about all three body axes. The results showed that by using a hodograph presentation of rate of descent and circumferential velocity, an altimeter, and vehicle attitude and rate meters, the pilots could consistently establish final altitude and velocity combinations that result in orbits lying within an altitude range of 10 to 90 miles above the lunar surface with a fuel consumption from 1 to 3 percent of the initial vehicle mass more than that required by the two-impulse Hohmann maneuver. (Author).
Human Factors Engineering Bibliographic Series
Author: Scientific and Technical Aerospace Reports
Author: Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1284
Book Description