CV-990 Galileo II arrival at Ames after first expedition - decending ramp are from top Don Anderson, Mike Bader, Hans Mark

The Ames spirit of free and vigorous discussion; Left to right: R. T. Jones, Jack Nielsen, Hans Mark, Leonard Roberts and Harvey Allen during an award ceremony honoring R.T. Jones.

F-18 HICL II model in 12ft w.t.

F-18 HICL II model in NASA Ames Research Center 12ft Pressure Wind Tunnel 12ft w.t.

CV-990 (NASA-712) Galileo II aircraft in flight over the San Francisco's Golden Gate Bridge. A digital navigation, guidance and autopilot system tested on Galileo 1 and Galileo II in 1975 looked at the feasibility of energy-management approach concepts for an unpowered vehicle. Flight tests carried out by pilot Fred Drinkwater with technical direction by Fred Edwards and John D Foster along with significant input from Gordon Hardy on the pilot's system interface. Note: Used in publication in Flight Research at Ames; 57 Years of Development and Validation of Aeronautical Technology NASA SP-1998-3300 fig 95 ref 99

The Ames spirit of free and vigorous discussion; Left to right: Harv Lomax, Leonard Roberts and Harvey Allen during an award ceremony honoring R.T. Jones.

Olczak Bell X-14 AIRCRAFT TWENTIETH ANNIVERSARY. Research Team: Front Row: Fred Drinkwater, Jim Meeks, Lonnie Phillips, Jim Kozalski, Vic Bravo. Second Row: Bill Carpenter, Sid Selan, Dick Gallant, Terry Stoeffler. Third row: Ron Gerdes, Lloyd Corliss. Fourth row: Cy Sewell, Dick Greif, Ed Vernon, Lee Jones. Fifth Row: Dan Dugan, Jim Rogers, Dave Walton, Terry Feistel. Back Row: Frank Pauli, Seth Anderson. Not pictured: Terry Gossett, Bob Innis, Stew Rolls, Lawson Williamson. Note: Used in publication in Flight Research at Ames; 57 Years of Development and Validation of Aeronautical Technology NASA SP-1998-3300 fig. 118

1/5th scale model of the 80x120ft w.t. in N-246

4' and 24' Shock Tubes - Electric Arc Shock Tube Facililty N-229 (East) The facility is used to investigate the effects of radiation and ionization during outer planetary entries as well as for air-blast simualtion which requires the strongest possible shock generation in air at loadings of 1 atm or greater.

CV-990 Galileo II arrival at Ames after first expedition - decending ramp are from top Don Anderson, Mike Bader, Dean Chapman (?), Hans Mark and unknown

NASA/NAVAIR Marine AV-8B aircraft test-493 in 40x80ft. w.t.

NASA/US Army Multcyclic test rotor in the Ames 40x80ft. Subsonic Wind Tunnel, Ames Research Center, Moffett Field, CA with John Bouldt.

Space Shuttle Tile Thermal Protection System testing in Ames Arc Jet facilities

Space Shuttle Tile Thermal Protection System testing in Ames Arc Jet facilities

NASA/NAVAIR Marine AV-8B aircraft test-493 in 40x80ft. w.t.

CV-990 Galileo II arrival at Ames after first expedition

BetaCom 700H computer graphic systems in N-233 with Thomas Crawford

NASA/NAVAIR AV-8B aircraft test-493 at Static Test Stand Facility

R.T. Jones with models

NASA/NAVAIR Marine AV-8B aircraft test-493 in 40x80ft. w.t.

C-8A (NASA-716) Buffalo Augmetor Wing Jet STOL Aircraft cockpit - SERVO installations

F-18 HICL II model in 12ft w.t.

QSRA (Quiet Short-Haul Research Aircraft) S-Duct Test: Static test facility installation (Appeared on the cover of the Avaiation Week & Space Technology on March 21, 1977)

Crows Landing Naval Auxiliary Landing Field and flight research facility, Crows Landing, CA Note: Used in publication in Flight Research at Ames; 57 Years of Development and Validation of Aeronautical Technology NASA SP-1998-3300 fig. 109

NASA/NAVAIR Marine AV-8B aircraft test-493 in 40x80ft. w.t. with test crew