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Displaying 9 of 9 results

Design of automation tools for management of descent traffic [microform] / Heinz Erzberger, William Nedell.

Text

Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1988]

1988

0 resources

Ascent/descent ancillary data production user's guide [microform] / prepared by H.R. Brans, A.W. Seacord, J.W. Ulmer.

Text

Houston, Tex. : System Development Division, TRW Defense Systems Group ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]

1986

0 resources

Calculation of water drop trajectories to and about arbitrary three-dimensional bodies lifting and nonlifting bodies in potential airflow [microform] / Hillyer G. Norment.

Text

[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1985.

1985

0 resources

Descent strategy comparisons for TNAV-equipped aircraft under airplane-preferred operating conditions [microform] / K.H. Izumi.

Text

[Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.

1989

0 resources

Capture conditions for merging trajectory segments to model realistic aircraft descents [microform] / Yiyuan Zhao and Rhonda A. Slattery.

Text

Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

1996

0 resources

Near-optimal re-entry trajectories for reusable launch vehicles [microform] / H.-C. Chou and M.D. Ardema, and J.V. Bowles.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Comparison of nonequilibrium solution algorithms applied to chemically stiff hypersonic flows [microform] / G. Palmer and E. Venkatapathy.

Text

Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

1995

1 resource

Available online

http://purl.access.gpo.gov/GPO/LPS54368

Minimum-cost aircraft descent trajectories with a constrained altitude profile / Minghong G. Wu, Alexander V. Sadovsky.

Text

Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, April 2015.

2015-4

1 resource

Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / Parviz A. Bahrami.

Text

Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012.

2012

1 resource

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