Low- and high-altitude tests of parachutes designed for use in low-density atmospheres
Parachutes for low density atmospheres, describing low and high altitude test results
Eckstrom, C. V.↗
Engineering topics
Eckstrom, C. V.
Publications and source records attributed to Eckstrom, C. V..
High-altitude flight test of a 40-foot- diameter /12.2-meter/ ringsail parachute at a deployment Mach number of 2.95
High altitude flight test of ringsail parachute with deployment at Mach 2.95
Eckstrom, C. V.↗
Flight test of a 40 foot nominal diameter disk-gap-band parachute deployed at a Mach number of 3.31 and a dynamic pressure of 10.6 pounds per square foot
Performance test on disk gap band parachute at supersonic speeds
Eckstrom, C. V.↗
Flight-test results from supersonic deployment of an 18-foot-diameter /5.49 meter/ towed ballute decelerator
Supersonic deployment and extraction of inflatable towed ballute decelerator
Eckstrom, C. V.↗
Flight test of a 40-foot-nominal-diameter disk-gap-band parachute deployed at a Mach number of 2.72 and a dynamic pressure of 9.7 pounds per square foot
Flight test of 40 foot parachute deployed at low supersonic speed and dynamic pressure
Eckstrom, C. V.↗
Flight test of a 40-foot nominal diameter disk gap band parachute deployed at a Mach number of 1.91 and a dynamic pressure of 11.6 pounds per square foot
Flight test of l0-foot nominal-diameter disk-gap band parachute to determine deployment and inflation, opening shock loads, drag efficiency, and stability characteristics
Eckstrom, C. V.↗
Flight test of a 30 foot nominal diameter cross parachute deployed at a Mach number of 1.57 and a dynamic pressure of 9.7 pounds per square foot
Flight test of 30 foot nominal diameter cross parachute to measure shock loads, drag efficiency, and stability characteristics
Eckstrom, C. V.↗
Flight test of a 40-foot-nominal-diameter modified ringsail parachute deployed at a Mach number of 1.64 and a dynamic pressure of 9.1 pounds per square foot
Flight tests of ringsail parachute with 15 percent porosity, for planetary entry
Eckstrom, C. V.↗
Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot
Flight test of disk-gap band parachute deployed at low supersonic speed and low dynamic pressure to obtain performance data on planetary entry parachute configurations
SUPERSONIC SPEED↗
Flight test of a 31.2-foot-diameter modified ringsail parachute deployed at a Mach number of 1.39 and a dynamic pressure of 11.0 pounds per square foot
Flight test of 31.2-foot-diameter modified ringsail parachute deployed at Mach 1.39 and dynamic pressure of 11 pounds per square foot
FLIGHT TEST↗
Development and testing of the disk-gap-band parachute used for low dynamic pressure applications at ejection altitudes at or above 200,000 feet
Development and flight test of inflatable disk- gap-band parachute for high altitude deployment from sounding rockets
SOUNDING ROCKET↗
Description of a new parachute designed for use with meteorological rockets and a consideration of improvements in meteorological measurements.
Parachute for meteorological rockets, noting design, testing, high altitude performance, etc
PARACHUTE FABRIC↗
Theoretical study and engineering development of jimsphere wind sensor final report, 27 feb. 1964 - 1 jun. 1965
Fabrication and flight tests of Jimsphere wind sensor balloons
BALLOON FLIGHT↗
Theoretical study and engineering development of Jimsphere Wind Sensor Final report, 27 Feb. 1964 - 1 Jun. 1965
Jimsphere wind measurement balloon flight test to determine optimum design for flow separation control and wake stabilization
WIND MEASUREMENT↗
Investigation of the flight characteristics of free flying aerodynamically shaped balloons Final report
Flight characteristics of free flying aerodynamically shaped balloons
AERODYNAMIC CHARACTERISTICS↗