Small rockets for experiments at high levels

Details Small rockets for experiments at high levels Small rockets for experiments at high levels

Jun 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978esasp.135..407f&link_type=abstract

In ESA European Sounding Rocket, Balloon and Related Res., with Emphasis on Expt. at High Latitudes p 407-409 (SEE N79-31637 2

Computer Science

Sound

Aerodynamic Drag, Design Analysis, Economic Factors, Solid Propellant Rocket Engines, Sounding Rockets, Thermal Stresses, Aerodynamic Characteristics, Apogees, Heat Shielding, Multistage Rocket Vehicles, Outgassing

Scientific paper

The aerodynamic drag and structural heating of rockets for research are discussed in the context of the requirements for conductive surfaces and avoidance of outgassing. Drag curves are presented which are basically applicable to any rocket with any number of stages. Economic advantages in the use of small rockets are emphasized and illustrated by examples. Efficiency curves for sounding rockets as a function of stage size distribution are given. Available motors for multistage rockets are reviewed.

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