Subcompact vehicle energy absorbing column evaluation and improvement. Volume I: analysis of accident data, engineer's point of view. Interim report.

National Highway Traffic Safety Administration, Washington, D.C.

Vehicle component characterization. Volume II - data appendices. Final report.

National Highway Traffic Safety Administration, Office of Research and Development, Washington, D.C.

Evaluation and correlation of driver/vehicle data. Volume I: summary report.

National Highway Traffic Safety Administration, Washington, D.C.

Evaluation and correlation of driver/vehicle data. Volume III: literature survey.

National Highway Traffic Safety Administration, Washington, D.C.

High occupancy vehicle treatments, impacts and parameters. Volume II - bibliography and data. Final report.

Mode of access: Internet.

Analysis of Madison County vehicle data to evaluate the effect of Autocheck program on vehicle accident rates. Final report.

National Highway Traffic Safety Administration, Washington, D.C.

Development of a motor vehicle materials historical high-volume industrial processing rates cost data bank (3500-4000 pound) full size car. Final report.

National Highway Traffic Safety Administration, Washington, D.C.

Disaggregated financial data and analysis for the domestic motor vehicle manufacturers. NHTSA technical report.

National Highway Traffic Safety Administration, Washington, D.C.

Analysis of missile trajectory measurement accuracy for data processing

"Contract no. AF 30(602)-2138, Project 5554, Task 55102."

A study of reconnaissance data from a boostglide vehicle. Contract no. AF30 (602)-2183, Rome Air Development Center.

"TR no. 61-51."

Illinois motor vehicle travel and related data.

Mode of access: Internet.

Development of a motor vehicle materials historical high-volume industrial processing rates cost data bank (3500-4000 pound) full size car /

Mode of access: Internet.

Flight data analysis of the HyShot 2 scramjet flight experiment

The development of scramjet propulsion for alternative launch and payload delivery capabilities has been composed largely of ground experiments for the last 40 years. With the goal of validating the use of short duration ground test facilities, a ballistic reentry vehicle experiment called HyShot was devised to achieve supersonic combustion in flight above Mach 7.5. It consisted of a double wedge intake and two back-to-back constant area combustors; one supplied with hydrogen fuel at an equivalence ratio of 0.34 and the other unfueled. Of the two flights conducted, HyShot 1 failed to reach the desired altitude due to booster failure, whereas HyShot 2 successfully accomplished both the desired trajectory and satisfactory scramjet operation. Postflight data analysis of HyShot 2 confirmed the presence of supersonic combustion during the approximately 3 s test window at altitudes between 35 and 29 km. Reasonable correlation between flight and some preflight shock tunnel tests was observed.