论文信息 - Water pressure and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system - 字舞流文

Water pressure and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system

Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module with deployed heat shield impact attenuation system

[1] John R. McGehee,et al. Water-Landing Characteristics of a Reentry Capsule , 1959 .

[2] Sandy M. Stubbs. Landing characteristics of the Apollo spacecraft with deployed-heat-shield impact attenuation systems , 1966 .

[3] Sandy M. Stubbs. Dynamic model investigation of water pressures and accelerations encountered during landings of the Apollo spacecraft , 1967 .

[4] William C. Thompson. Dynamic Model Investigation of the Landing Characteristics of a Manned Spacecraft , 1964 .

[5] Sandy M. Stubbs. Landing Characteristics of a Re-entry Vehicle with a Passive Landing System for Impact Alleviation , 1963 .