Alternate stage of the Soviet space program - Controlled descent of ''Zond-6'' from the path earth-moon-earth
Zond-6 circumlunar flight and controlled descent landing in U.S.S.R.
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Zond-6 circumlunar flight and controlled descent landing in U.S.S.R.
Pathfinding algorithm for unmanned roving vehicle to explore Martian surface
Discrete change in ballistic coefficient for trajectory control in Mars entry guidance
Scintillation of ground based spherical wave laser source viewed from space analyzed from Geos 2 satellite laser tracking, noting stellar scintillation correspondence
Maximum trajectory for glider entering earth atmosphere at supercircular velocity, subject to maximum altitude constraint
High voltage ionization of gases in shock tubes by arc discharges
Computerized simulation of terrain sensing and modeling for unmanned surface vehicle on Mars surface
Table structure and rotating magnet system simulating gravitational forces on spacecraft and displaying trajectories between Earth, Venus, and Mercury
Method and apparatus for producing fine particles in cryogenic liquid bath for gelled rocket propellants
Determination of orbit estimates for Mariner 6 and 7 space probe flights
Solder coating process for printed copper circuit protection
Open circuit and bias degradation tests in copper and cadmium sulfide thin film solar cells
High efficiency transformerless amplitude modulator coupled to RF power amplifier
Development of method and apparatus for spinning satellite about selected axis after reaching predetermined orientation
Analysis of typical Jupiter-Saturn-Pluto trajectory to determine characteristics of outer planet space missions and planetary quarantine constraints
Planetary quarantine constraint on 1977 Jupiter- Saturn-Pluto mission, determining fuel loading penalties, optimum biasing strategies and outer planet navigational characteristics
SDS-930 computer determines impact cost-decision value at any chronological point in definition phase of multiprogram project. Options, option combinations, and different displays are listed. Graphical procedure was chosen as best method for project.