M. E. Nichols

发表

Results of investigations on an 0.015-scale configuration 140A/B space shuttle vehicle orbiter model (49-0) in the NASA/Langley Research Center 8-foot transonic pressure tunnel (OA25)

M. E. Nichols, 1974 .

The Development of Algorithms For Neutron-Based Threat Determinations

Phillip C. Womble, M. E. Nichols, Alexander Barzilov, 2007 .

Results of investigations (OA20C) on an 0.015-scale configuration 140A/B space shuttle vehicle orbiter model (49-0) in the NASA/Langley Research Center Unitary Plan Wind Tunnel

M. E. Nichols, 1974 .

Investigations to the space shuttle orbiter 2A configuration 0.015-scale model in the NASA Ames Research Center 3.5-foot hypersonic wind tunnel at Mach numbers 5, 7 and 10 (OA11B)

M. E. Nichols, M. D. Milam, J. A. Mellenthin, 1974 .

Investigations on an 0.030-scale space shuttle vehicle configuration 140A/B orbiter model in the Ames Research Center unitary plan 8 by 7-foot supersonic wind tunnel (0A53C)

M. E. Nichols, 1974 .

Investigations of the 0.020-scale 88-OTS Integrated Space Shuttle Vehicle Jet-Plume Model in the NASA/Ames Research Center 11 by 11-Foot Unitary Plan Wind Tunnel (IA80). Volume 4

M. E. Nichols, 1976 .

Results of investigations conducted in the LaRC 8-foot transonic pressure tunnel using the 0.010-scale 72-OTS model of the space shuttle integrated vehicle (IA93), volume 2

M. E. Nichols, 1976 .

Results of flow-visualization investigations on a 0.015-scale modified configuration 140A/B space shuttle vehicle orbiter (model 36-0) in the Langley Research Center 8-foot transonic pressure tunnel (OA102)

M. E. Nichols, 1975 .

Results of investigations (OA20A) on a 0.015-scale 140A/B configuration space shuttle vehicle orbiter model in the NASA/Langley Research Center unitary plan wind tunnel

M. E. Nichols, 1974 .

Results of investigations conducted in the LaRC 4-foot unitary plan wind tunnel leg no. 1 using the 0.010-scale 72-OTS model of the space shuttle integrated vehicle (IA94A)

M. E. Nichols, 1976 .

Applications for satellite positioning technology in the construction industry

M. E. Nichols, 1996, Proceedings of Position, Location and Navigation Symposium - PLANS '96.

Results of investigations on a 0.015-scale model 2A configuration of the Rockwell International space shuttle orbiter in the NASA/Ames Research Center 3.5 foot hypersonic wind tunnel

M. E. Nichols, M. D. Milam, J. A. Mellenthin, 1973 .

Static and control investigations of an 0.030-scale space shuttle orbiter configuration 140A/B model in the Ames Research Center 11 by 11-foot transonic wind tunnel (OA53A), Volume 1

M. E. Nichols, 1974 .