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4 research outputs found

TOLIP - Trajectory optimization and linearized pitch computer program

Author: Rosenbaum R. C.
Willwerth R. E., Jr.
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Trajectory optimization and linearized pitch computer program for Scout launch vehicl

NASA Technical Reports Server

Mars Surface-to-Orbit Vehicles for Sample Return Missions

Author: WILLIAM L. WEAVER
Willwerth R. E. Jr.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
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Field of study

Optimal payload trajectory characteristics for horizontally launchedbooster vehicle.

Author: Brockway D. J.
In
JARRELL R. ELLIOTT
Penner S. S.
Sandri R.
Teren F.
TIMOTHY R. RAU
Willwerth R. E. Jr.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
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Field of study

Experience using Balakrishnan's epsilon technique to compute optimumflight profiles

Author: Balakrishnan A. V.
Balakrishnan A. V.
Bellman R.
Cockayne W. G.
HARRIET J. SMITH
KENNETH W. ILIFF
LAWRENCE W. TAYLOR
Lush K. J.
Matthews M. L.
Rempfer P. S.
Schmidt H. E.
Stein L. H.
Willwerth R E., Jr.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
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