A five-stage solid-fuel sounding-rocket system which can boost a payload of 25 pounds to an altitude of 525 nautical miles and that of 100 pounds to 300 nautical miles is described. Data obtained from a typical flight test of the system are discussed
Missions currently being considered by NASA beyond the Apollo manned lunar landing will require a la...
Static stability of single-stage meteorological sounding rocket at Mach numbers from 6.0 to 12.
Sounding rockets are unique experimental platforms! They are unmanned, readily available, cost-effec...
A flight investigation of two Nike-Deacon (DAN) two-stage solid-propellant rocket vehicles indicated...
Use of high-performance aircraft as first-stage booster for air-launching solid fuel rocket - operat...
Sounding rockets for transporting scientific instruments in nearly vertical trajector
Radio-attenuation measurement /ram a1/ test, four- stage solid-propellant rocket vehicle - performan...
Current efforts by the student members of the sole student rocket group at Arizona State University,...
Sounding rockets are rocket vehicles designed to carry scientific payloads above the sensible level ...
Solid propellant rocket systems design and combustion efficiency and burning rate of solid propellan...
http://deepblue.lib.umich.edu/bitstream/2027.42/5373/5/bad5733.0001.001.pdfhttp://deepblue.lib.umich...
In-situ measurements in middle and higher atmosphere regions are often only possible by means of sou...
The effect on performance of variations in power plant, aircraft, and rocket parameters was calculat...
A Nike-Cajun (CAN) two-stage solid-propellant rocket vehicle was flight tested for performance. This...
A compilation of weight, balance, center of gravity, and moments of inertia of various sounding rock...
Missions currently being considered by NASA beyond the Apollo manned lunar landing will require a la...
Static stability of single-stage meteorological sounding rocket at Mach numbers from 6.0 to 12.
Sounding rockets are unique experimental platforms! They are unmanned, readily available, cost-effec...
A flight investigation of two Nike-Deacon (DAN) two-stage solid-propellant rocket vehicles indicated...
Use of high-performance aircraft as first-stage booster for air-launching solid fuel rocket - operat...
Sounding rockets for transporting scientific instruments in nearly vertical trajector
Radio-attenuation measurement /ram a1/ test, four- stage solid-propellant rocket vehicle - performan...
Current efforts by the student members of the sole student rocket group at Arizona State University,...
Sounding rockets are rocket vehicles designed to carry scientific payloads above the sensible level ...
Solid propellant rocket systems design and combustion efficiency and burning rate of solid propellan...
http://deepblue.lib.umich.edu/bitstream/2027.42/5373/5/bad5733.0001.001.pdfhttp://deepblue.lib.umich...
In-situ measurements in middle and higher atmosphere regions are often only possible by means of sou...
The effect on performance of variations in power plant, aircraft, and rocket parameters was calculat...
A Nike-Cajun (CAN) two-stage solid-propellant rocket vehicle was flight tested for performance. This...
A compilation of weight, balance, center of gravity, and moments of inertia of various sounding rock...
Missions currently being considered by NASA beyond the Apollo manned lunar landing will require a la...
Static stability of single-stage meteorological sounding rocket at Mach numbers from 6.0 to 12.
Sounding rockets are unique experimental platforms! They are unmanned, readily available, cost-effec...