Planetary entry parachute testing using a balloon as a launch platform
Planetary entry parachute testing using balloon as launching platform
BALLOON↗
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Results for “entry”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Positional relation of spermium point of entry to the median plane and to the primitive groove after local vital staining tests with the axolotl ovum
Positional relation of spermium point of entry to median plane and to primitive groove after local vital staining tests with axolotl ovum
AMPHIBIA↗
Entry acquisition and radio visibility computer program
Entry acquisition and radio visibility computer program for optimization of tracking station locations - blackout prediction
COMPUTER PROGRAM↗
Voyager capsule, preliminary design, phase B. Volume IV - Entry science package. Section II - Preliminary design for OSE FINAL report
Operational support equipment preliminary design for entry science package portion of Voyager flight capsule system
GROUND SUPPORT EQUIPMENT↗
Voyager capsule, preliminary design, phase B. Volume IV - Entry science package. Section V - Interfaces Final report
Hardware, software, and service interfaces between capsule bus, entry science package, and Voyager spacecraft
SPACE CAPSULE↗
Voyager capsule phase B. Volume IV - Entry science package. Part A - Introduction and summary. Part B - Mission objectives and requirements. Part C - Constraints. Part D - Selected design concepts Final report
Objectives, constraints, and design of Voyager entry science package for Mars atmosphere probe
VOYAGER PROJECT↗
Voyager capsule phase B. Volume IV - Entry science package. Part E - Alternatives and systems analysis. Part F - Future mission options Final report
Design alternatives and systems analysis of Voyager entry science package for Mars atmosphere probe
EXPERIMENT DESIGN↗
Voyager capsule phase B. Volume IV - Entry science package. Part G - Subsystem/equipment descriptions Final report
Major equipment and subsystem descriptions of Voyager entry science package for Mars
SPACECRAFT DESIGN↗
Voyager capsule phase B. Volume IV - Entry science package. Part H - Reliability. Part I - Planetary quarantine, Part J - Operational support equipment. Part K - Interface alternatives Final report
Reliability, planetary quarantine, support equipment, and interface alternatives of Voyager entry science package for Mars atmosphere probe
COMPONENT RELIABILITY↗
Lifting entry vehicles for future space missions.
Lifting entry vehicles requirements for near earth and planetary missions, noting four thermal protection systems
THERMAL PROTECTION↗
Entry of solar cosmic rays into the polar cap atmosphere.
Three stages of solar cosmic rays entry into polar cap atmosphere due to differential arrival of solar electrons, protons and alpha particles
SOLAR COSMIC RAY↗
Electrodeless magnetogasdynamic power during entry.
Electrodeless MGD power generation during entry, using torque on magnet taken as rotating member of generator
POWER GENERATOR↗
Importance of recovery-site location in determining entry vehicle requirements for future missions.
Recovery site location importance in determining entry vehicle future requirements
LIFTING BODY↗
High-altitude hypersonic flow effects on the lateral range capability of entry vehicles.
High altitude hypersonic viscous flow degradation of L/D effects on entry vehicle lateral range capability
VISCOUS FLOW↗
Advanced materials and structures for entry systems.
Materials and structural concepts for design of entry systems, discussing environmental factors, reuse potential and high reliability
SPACECRAFT CONSTRUCTION MATERIAL↗
Interplanetary guidance systems requirements study. Volume 2 - Computer program descriptions. Part 5 - Nominal atmospheric entry trajectories, version 1
Computer program for simulating lifting vehicle atmospheric entry flight trajectory
Source record↗
Interplanetary guidance system requirements study. Volume 2 - Computer program descriptions. Part 7 - Performance assessment of atmospheric entry guidance systems
IBM 7094 computer program for simulating atmospheric entry aided-inertial guidance systems
Source record↗
Study, definition and analysis of pilot/system performance measurements for planetary entry experiments
Definition analysis for experimental prediction of pilot performance during planetary entry
Johnston, D. E.↗