Measurement of upper atmospheric ionization and winds with a combined payload Interim report
Sounding rocket flights for determining structure of electron density profile and wind in E region
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Sounding rocket flights for determining structure of electron density profile and wind in E region
Measurements on ultraviolet fluxes from stars and nebulosities by rockets carrying photomultiplier and ionization chamber detectors
Aerobee 350 with Nike booster launched for engineering - space science research
Trajectory energy requirements for low-thrust flights throughout solar system using nuclear- electric propulsion
Particulate contamination control of ultraclean collecting surface for extraterrestrial matter in Aerobee 150
Computer programs for synthesizing structural arrangements for ring-stiffened, honeycomb sandwich, and ring-stringer stiffened methods of construction for Saturn nose fairings
Launch vehicle systems safety engineering requirements and procedures at contractor and subcontractor level
Science experiments, photoimaging equipment, and Voyager spacecraft configurations for studying Mars atmosphere and surface temperature
Azimuth sensing system for continuous, ground monitoring of azimuth orientation for Planetary Entry Parachute Program /PEPP/ spacecraft
Cosmic ray anisotropy instrument aboard Pioneer 8 featuring computer for azimuth determination, data compression and detector control
Active control techniques to isolate flexible system from LF vibration disturbances, transient response damping and isolator static deflections minimization
Combined range rate and telemetric interferometer system for radar tracking of scientific sounding rockets
Evaluating effects of surface protuberances on impact limiters on hard landings by impact tests
Design development discussion of primate support system for Biosatellite
Command and control system for real-time operation of Surveyor spacecraft
GE-RESD primate life support subsystem design for NASA-ARC biosatellite program
Aerodynamic force and moment coefficients for scale model of expendable second stage modified S-2 alone and mounted piggyback on space shuttle booster from Mach 0.6 to 4.96
Design and operation of the primate life support subsystem for the Biosatellite Program as used during the flight of Biosatellite 3 are discussed. Included are preflight changes necessitated by the primate's (a Macaca nemistrina monkey) influence on the initial equipment design.