Test facility for simulation of system- environment interaction during Martian entry.
Martian entry test facility for real size entry systems, discussing design, fabrication and operation
Berry, G. A.↗
Engineering topics
Heer, E.
Publications and source records attributed to Heer, E..
Optimum structural design based on reliability analysis
Space vehicle optimal design based on reliability analysis, taking into account cost of materials strength tests
Heer, E.↗
Aeroshell structural development for Martian entry.
Aeroshell structural development for Mars flyby and entry landing mission compatible with Atlas/Centaur launch vehicle
Garba, J. A.↗
Receptance coupling of structural components near a component resonance frequency
Receptance coupling of structural components near resonance frequency
Heer, E.↗
Analysis of space vehicle structures using the transfer-function concept.
Frequency transfer function applied to space vehicle structural analysis
Heer, E.↗
Stress analysis of solid propellant rocket motors
Linear viscoelastic and elastic problem in stress analysis of solid propellant rocket engines
Akyuz, F. A.↗
The production of charged pions by 600 MeV protons on various nuclei
Charged pion production by proton beam incidence on elements from beryllium to lead
NUCLEAR SCATTERING↗