Add to ORKGThe design is described of the Venus probe windows, which are required to measure solar flux, infrared flux, aureole, and cloud particles. Window heating and structural materials for the probe window assemblies are discussed along with the magnetometer. The command lists for science, power and communication requirements, telemetry sign characteristics, mission profile summary, mass properties of payloads, and failure modes are presented
The Pioneer Venus mission study was conducted for a probe spacecraft and an orbiter spacecraft to be...
A summary of the spacecraft descriptions; the probe bus, large probe, small probe, and orbiter is pr...
Structural design, systems and subsystems requirements, entry probe configurations, and transfer tra...
Power subsystem cost/weight tradeoffs are discussed for the Venus probe spacecraft. The cost estimat...
Pioneer Venus spacecraft performance requirements are presented. The specifications include: (1) Des...
The NASA Ames Research Center Pioneer Venus Project objective is to conduct scientific investigation...
The results are reported of the Pioneer Venus studies from 2 October 1972 through 30 June 1973. Many...
The objectives of the low-cost Pioneer Venus space probe program are discussed. The space mission an...
The procedures for predicting the aeroheating environment of Venus entry probes are outlined. After ...
Selection of a baseline power subsystem for the probe bus, orbiter, and large and small probes has b...
The aerodynamic design problems for the Pioneer Venus mission are discussed for a small probe shape ...
The requirements, trades, and design descriptions for the probe bus and orbiter spacecraft configura...
The mission, systems, operations, ground systems, and reliability analysis of the Thor/Delta baselin...
Communications subsystem tradeoffs were undertaken to establish a low cost and low weight design con...
Study tasks for the command and data handling subsystems have been directed to: (1) determining grou...
The Pioneer Venus mission study was conducted for a probe spacecraft and an orbiter spacecraft to be...
A summary of the spacecraft descriptions; the probe bus, large probe, small probe, and orbiter is pr...
Structural design, systems and subsystems requirements, entry probe configurations, and transfer tra...
Power subsystem cost/weight tradeoffs are discussed for the Venus probe spacecraft. The cost estimat...
Pioneer Venus spacecraft performance requirements are presented. The specifications include: (1) Des...
The NASA Ames Research Center Pioneer Venus Project objective is to conduct scientific investigation...
The results are reported of the Pioneer Venus studies from 2 October 1972 through 30 June 1973. Many...
The objectives of the low-cost Pioneer Venus space probe program are discussed. The space mission an...
The procedures for predicting the aeroheating environment of Venus entry probes are outlined. After ...
Selection of a baseline power subsystem for the probe bus, orbiter, and large and small probes has b...
The aerodynamic design problems for the Pioneer Venus mission are discussed for a small probe shape ...
The requirements, trades, and design descriptions for the probe bus and orbiter spacecraft configura...
The mission, systems, operations, ground systems, and reliability analysis of the Thor/Delta baselin...
Communications subsystem tradeoffs were undertaken to establish a low cost and low weight design con...
Study tasks for the command and data handling subsystems have been directed to: (1) determining grou...
The Pioneer Venus mission study was conducted for a probe spacecraft and an orbiter spacecraft to be...
A summary of the spacecraft descriptions; the probe bus, large probe, small probe, and orbiter is pr...
Structural design, systems and subsystems requirements, entry probe configurations, and transfer tra...