DSIF IN THE RANGER PROJECT
Deep space instrumentation facility /dsif/ in ranger project
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Deep space instrumentation facility /dsif/ in ranger project
Analysis of Deep Space Instrumentation Facility tracking performance during Ranger VII mission
Computer program for analysis or design of carrier tracking or clock tracking loops of Deep Space Instrumentation Facility receiver
Reliability efforts and test facility developments summarized for Deep Space Instrumentation Facility and Surveyor, Mariner, and Voyager projects
Error sources associated with Doppler radar tracking data of lunar satellite orbits taken by Deep Space Instrumentation Facility
Space flight operations - launch site, deep space instrumentation facility, operations complex, launch site, communications facility, and checkout facility
Modified root-mean-square computer program used to evaluate distortion of reflective surface of paraboloidal antenna - Deep Space Instrumentation Facility /DSIF/
At the Project Design Center at the Jet Propulsion Laboratory, a concurrent design environment is under development for supporting development and analysis of space instruments and telescopes in the early, conceptual design phases.
The CALorimetric Electron Telescope CALET is a space instrument designed to carry out precision measurements of high energy cosmic-rays on the JEM-EF external platform on the International Space Station, where it has been collecting science data continuously since mid-October 2015. In addition to its primary goal of identifying nearby sources of high-energy electrons and possible signatures of dark matter in the electron spectrum, CALET is carrying out extensive measurements of the energy spectra, relative abundances and secondary-to-primary ratios of elements from proton to iron, and even above (up to Z = 40), studying the details of galactic particle propagation and acceleration. An overview of CALET based on the data taken during the first three years of observations is presented, including a direct measurement of the electron+positron energy spectrum from 11 GeV to 4.8 TeV. The proton spectrum has been measured from 50 GeV to 10 TeV covering, for the first time with a single space-borne instrument, the whole energy interval previously investigated in separate sub-ranges by magnetic spectrometers and calorimetric instruments. Preliminary spectra of cosmic-ray nuclei are also presented, together with gamma-ray observations and searches for an e.m. counterpart of LIGO/ Virgo GW events.
Deep space instrumentation facility /dsif/ spacecraft tracking performance during ranger iv lunar probe mission
DSN functions and facilities, including Deep Space Instrumentation Facility, Ground Communications Facility, and Space Flight Operations Facility
Hermetically sealing a gas tank and opening it into tubing under telecommand control is a function required in various space instruments. There are a number of space valves that are power saving, withstand vibration, and do not contaminate the gas. But none of them combines these features with low mass and the ability to withstand temperatures of 130 C during the sterilization process mandatory for planetary missions. In this paper, a novel miniature valve is presented, which is particularly adapted to space applications. It is electrically actuated, utilizing a bimetallic snap-disc that pierces a metallic membrane by a needle pin, thereby opening the valve. The design of this single-shot valve is such that it allows it to withstand a temperature of 130 C and a pressure of 50 bars. The valve is also lightweight (6.62 g) and it requires only 9 W to operate.
Deep space instrumentation facility tracking and data acquisition for Ranger missions VI-IX
Mariner Venus and Ranger tracking, examining quantization and transmitter stability as dominant effects in HF noise component of Deep Space Instrumentation Facility /DSIF/ L-band Doppler
Mark 1 ranging subsystem special purpose version of MOD II ranging equipment used in Deep Space Instrumentation Facility /DSIF/
Deep Space Instrumentation Facility two-way Doppler accuracy limitations - effect of charged particles
Deep Space Instrumentation Facility station control and data equipment
Deep Space Instrumentation Facility FR-900 ROTARY head magnetic tape recorders for acquiring video data from lunar orbiter