vania-janet/multiturn-rag-retrieval-data huggingface dataset:
Virtual Vocabulary | NASA eClips
Wind and water often carry sand and mud particles from one place and later deposit them somewhere else. What they drop off is called a deposit (so deposit is both a verb and a noun). topdesign - A design is a plan or drawing made to show the look and function of a spacecraft, building, garment, or other object before it is built or made. topdesign process - The design process is a series of steps in designing and refining/improving something. Steps of the Design Process 1. Identify the problem 2. Identify criteria and constraints 3. Brainstorm possible solutions 4. Generate ideas 5. Explore possibilities 6. Select a design 7. Build a model or prototype 8. Refine the design, repeating steps 1-8 topdetection - Detection is the process of identifying the presence of something such as a fire. topdiameter - Diameter is a straight line passing from side-to-side through the center of a body or figure like a circle or sphere. topdiffraction grating - A diffraction grating is a surface with many closely spaced parallel grooves or splits in it which splits and diffracts light to produce the light's spectrum. topdirection - Direction is the line or course on which something is moving. topdirt - Dirt is made of small particles formed from the breakdown of rocks. topdispatching system - A dispatching system receives 911 calls and notifies the emergency service (for example, fire department) of the location and nature of the emergency. topdormant - Dormant is when an organism's physical activity, growth, and development are slowed or temporarily stopped to conserve energy in unfavorable conditions. topdouble refraction - Double refraction, also called birefringence, is a property of light in which a single ray of unpolarized light entering a certain medium is split into two rays, each traveling in a different direction. One ray is bent, or refracted, at an angle as it travels through the medium; the other ray passes through the medium unchanged. topdrag - Drag is the resistance on an object to movement through a fluid. It is a force that slows an object down.
Search | NASA Software Catalog
The SROMPy software package is a tool to solve the optimization problem efficiently to generate an SROM that can be used to propagate uncertainty through a given model.
 

 Open Source
 

 MFS-27332-1
 

 VLOADS V1.4 Launch Vehicle Loads Analysis For Preliminary Design
 

 The VLOADS program calculates launch vehicles' in-flight structural loads for preliminary design. The program may also be used to calculate structural loads for upper stages and planetary transfer vehicles. Launch vehicle information and input data such as aerodynamic coefficients, mass properties, propellants, engine thrusts, and performance data are compiled and analyzed by VLOADS to produce distributed shear loads, bending moments, axial forces, and vehicle line loads as a function of X-station along the vehicle's length. Translational accelerations and interface loads, if the launch vehicle has booseters or wings, are also computed.
 

 U.S. Release Only
 

 MFS-31223-1
 

 Monocoque Tank Analysis Spreadsheet System (MonTASS), Version 2.0
 

 The Monocoque Tank Analysis Spreadsheet System (MonTASS) computer program enables rapid analysis and preliminary design of structural domes and truncated sections of cones. MonTASS performs both design and analysis functions and can be used to analyze nonpressurized conical structures.
 

 U.S. Release Only
 

 LAR-16371-1
 

 Data Transfer Between Dissimilar Meshes (DTBDM, 2.0)
 

 Designed to automate an otherwise labor-intensive process, DTBDM puts the aerodynamic loads output of a computational fluid dynamics (CFD) package into the structural model of an aircraft to allow for deflection calculations.
 

 U.S. Release Only
 

 LEW-18460-1
 

 A Software Platform for Post-Processing Waveform-Based NDE - V2.0
 

 A Software Platform for Post-Processing Waveform-Based NDE - V2.0

The NDE Wave 
 

 U.S. Release Only
 

 LAR-19800-1
 

 PanNDE
 

 This disclosure describes software and its framework for physics-based simulation of nondestructive evaluation (NDE). The software is comprised of core plugin interfaces for mesh formats, simulation metadata, and simulation results.
Dr. James R. Drummond | Terra
An international leader in space instrument design, testing and deployment, Drummond is coming up with more effective and more comprehensive ways of monitoring the health of the atmosphere. By developing new, specialized instruments, Drummond and his colleagues are able to take better measurements of the gases and particles in the atmosphere and thus gain a deeper understanding of what is happening to the air. Their research is taking us one step closer to a time when we will have a continuous real-time picture of the atmosphere.
An extremely significant part of Dr. Drummond’s research effort in the last 30 years has been devoted to the Measurements Of Pollution In The Troposphere (MOPITT) instrument to measure carbon monoxide in the troposphere. The MOPITT project is directly funded by the Canadian Space Agency.
Drummond has been involved in a number of other projects including: Sub-Doppler Infrared Spectroscopic Studies of Line Shape and Broadening Mechanisms, the Middle Atmosphere Nitrogen Trends Assessment (MANTRA), the SCISAT program, a Mission to the Atmosphere of Mars, an Industrial Research Chair, a Canadian Research Chair, the Canadian Network for the Detection of Atmospheric Change (CANDAC), the Polar Environment Atmospheric Research Laboratory (PEARL) and the Canadian Network of Northern Research Operators (CNNRO).
Drummond has degrees in physics and atmospheric physics from Oxford University.

 

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Tools and Data Quick Reference | Terra
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Planetary Exploration Test Facilities | Glenn Research Center | NASA
Due to its particle shape, this material mimics the wind-blown dune soil on Mars and has extremely low shear strength, which produces a very challenging trafficability case for roving vehicles.

The SLOPE lab is equipped with 32 infrared OptiTrak motion tracking cameras; 20 are mounted permanently on the walls and 12 are on tripods, providing a full 360-degree field of view.  The test vehicles or subjects can be outfitted with trackers so that the rover position and orientation, with sub millimeter accuracy, can be captured in real time.
The VIPER Mobility Test Platform preparing to drive through a simulated crater
As mentioned above, the soil tanks in the SLOPE Lab are currently filled with two simulants:  GRC-1 lunar simulant, and Fillite high-sinkage medium.  GRC-1 is a custom poorly-graded soil consisting of semi-angular silica particles.  It was developed to match the bulk strength properties of the equatorial lunar terrain explored during the Apollo missions, with a focus on targeting the “softer”, more conservative range of properties with respect to vehicle mobility.  The soil density can be controlled providing a range of conditions. Fillite consists of hollow alumino-silicate microspheres and is intended to mimic the wind-blown dune soil found on Mars that has produced entrapped conditions for rovers.  Though the material is not a high-fidelity simulant, it has low bearing and shear strength, and produces a very challenging case for roving vehicles.  The material in the soil tanks can be changed out for alternate simulants upon request.
View a virtual tour of the SLOPE Lab.
TRaction and Excavation Capabilities (TREC) Rig
The TRaction and Excavation Capabilities (TREC) Rig is a single wheel dynamometer used to determine the tractive performance of various wheel and tire designs in simulated lunar and Mars soils. The TREC Rig offers independent motion control of the carriage and the tire such that forced slip conditions ranging from 0 to 90% can be achieved. The vertical tire load is adjustable from approximately 90 N to 900 N, including off-loading capability. The linear speed is also adjustable with a maximum rate of 6 cm/s. Tires up to 95 cm in diameter can be tested in the rig’s current configuration.
Audio and Ringtones - NASA
More Audible Sounds from InSight’s Seismometer on Mars

Listen to data from the seismometer on NASA’s InSight spacecraft of vibrations caused by Martian wind moving over the lander’s solar panels. In this version, the data have been processed to raise the frequencies by two octaves to make them more audible.

Sounds from InSight’s Pressure Sensor on Mars

Listen to data from the air pressure sensor on NASA’s InSight lander, indicating wind blowing by on Mars. The data were sped up by a factor of 100, shortening the duration of the recording and shifting it up in frequency 100 times (a little more than six octaves).

Third Rock Radio

NASA’s mission of discovery and exploration is being showcased in a custom-produced Internet music radio station that is crafted specifically to speak the language of tech-savvy young adults. Third Rock – America’s Space Station offers listeners a New Rock/Indie/Alternative format. The station is being developed and operated at no cost to the government through a Space Act Agreement with Houston-based RFC Media. Third Rock also will help partner companies fill high-tech job openings in the engineering, science and IT fields. Visit Third Rock.

Visit Third Rock

NASA on Soundcloud
A close-up view of an astronaut’s bootprint in the lunar soil, photographed with a 70mm lunar surface camera during the Apollo 11 extravehicular activity (EVA) on the moon. While astronauts Neil A. Armstrong, commander, and Edwin E. Aldrin Jr., lunar module pilot, descended in the Lunar Module (LM) “Eagle” to explore the Sea of Tranquility region of the moon, astronaut Michael Collins, command module pilot, remained with the Command and Service Modules (CSM) “Columbia” in lunar orbit.
Explore the universe and discover our home planet with NASA through a collection of our sounds from historic spaceflights and current missions. You can hear the roar of a space shuttle launch or Neil Armstrong’s “One small step for (a) man, one giant leap for mankind” every time you get a phone call if you make our sounds your ringtone.
Model Water Efficient Landscape Ordinance (MWELO) | Danville, CA
Limited size lawns and non-adapted plants can also be planted.Who needs to comply?Follow the Compliance Pathway Flowchart (PDF) for information about projects that need to comply.Any single-family or multi-family residential, public, institutional, or commercial project that requires a permit, plan review, or check from the local review agency AND meets one of these size thresholds needs to comply:New construction project with a total landscape area* greater than 500 sq. ft.Rehabilitation of existing landscape with a total landscape area* greater than 2,500 sq.ft.* Total landscape area includes swimming pools, fountains, and other water features.What is the Submittal, review, and approval process?Projects that meet the criteria above must comply with the  Town’s MWELO ordinance (which adopts the California MWELO ordinance) and  Bay-Friendly Basic Landscape Checklist (PDF). In order to achieve this, the following steps must be completed:Submitting your applicationPerformance Landscape Projects  Prior to construction, new construction projects 500 sq. ft. or larger or rehabilitated landscapes 2,500 sq. ft. or larger should submit: Performance Landscape Documentation Package (PDF)Water Allowance Worksheet (EXCEL)Soil Management ReportLandscape Design Plan Irrigation Design PlanGrading Design PlanPrescriptive Landscape ProjectsPrior to construction, rehabilitated projects between 500 sq. ft. and 2,500 sq. ft.
CALET
instrument was launched on August 19, 2015 by a Japanese carrier, 
H2 Transfer Vehicle (HTV), and robotically installed on the Japanese Experiment 
Module-Exposed Facility (JEM-EF) on the International Space Station (ISS).
First events were recorded in October 2015.
Mission Characteristics

 Lifetime : October 2015 – present

 Energy Range : 7 keV – 1 TeV

 Special Features : extremely high energy photon and cosmic ray particle detection

 Payload :

The CALET Calorimeter (CCAL) measures the cosmic-ray total electron 
 spectrum from energy ~1 GeV up to Tev region. It’s components are:
 
Charge Detector (CHD), a plastic scintillator hodoscope for 
 absolute charge measurement. It contains two orthogonal layers. 
 Each layer contains of 14 plastic scintillator paddles measuring
 45 x 3.2 x 1 cm. It can detect charge between 1 and ∼40 Z
 
IMaging Calorimeter (IMC), a sampling calorimeter. It consists of 
 16 kayers of scintillating fibers (SciFi) with 1 mm2
 cross section, with alternating layers arranged orthogonally. 
 It also includes interspacing thin tungsten absorbers, and tracks
 early show profile through the first 3 X0
Total AbSorption Calorimeter (TASC), a thick lead tungstate (PWO) 
 hodoscope with 12 alternating layers of X-Y arranged logs, with 
 a total shower depth of 27 X0

The CALET Gamma Ray Burst Monitor (CGBM) is sensitive from the 
 soft X ray (∼7 keV) to gamma ray (∼20 MeV) energy range.
 
Hard X-ray Monitor (HXR; two identical units) 
 
7 – 1000 keV
Lanthanum bromide (LaBr3(Ce)) scintillation detector
 61 mm diameter with 12.7 mm thick detector 
 ∼ 3 sr field of view
 
Soft Gamma-ray Monitor (SGM; one unit) 
 
100 keV – 20 MeV
Bismuth germanate (BGO) scintillation detector 
 102 mm diameter with 76 mm thick detector
 ∼ 8 sr field of view
NASA - NSSDCA - NMC - Data Collection - Query Results
Instrument (HRI)EPOXI C/GARRADD (2009 P1) - HRIV RAW IMAGES V1.0 (PDS)Deep Impact/EPOXI:High Resolution Instrument (HRI)EPOXI C/GARRADD (2009 P1) - HRIV CALIBRATED IMAGES V1.0 (PDS)Deep Impact/EPOXI:High Resolution Instrument (HRI)EPOXI C/GARRADD (2009 P1) - MRI RAW IMAGES V1.0 (PDS)Deep Impact/EPOXI:Medium Resolution Instrument (MRI)EPOXI C/GARRADD (2009 P1) - MRI CALIBRATED IMAGES V1.0 (PDS)Deep Impact/EPOXI:Medium Resolution Instrument (MRI)EPOXI 103P/HARTLEY2 ENCOUNTER - HRII CALIBRATED SPECTRA V3.0 (PDS)Deep Impact/EPOXI:High Resolution Instrument (HRI)EPOXI C/ISON (2012 S1) - HRII RAW SPECTRA V1.0 (PDS)Deep Impact/EPOXI:High Resolution Instrument (HRI)EPOXI C/ISON (2012 S1) - HRII
Audio and Ringtones - NASA
Cassini: Saturn Radio Emissions #1
Cassini: Saturn Radio Emissions #2
Juno: Morse code “HI” received from Earth
Kepler: Star KIC12268220C Light Curve Waves to Sound
Kepler: Star KIC7671081B Light Curve Waves to Sound
LCROSS: Water on the Moon Song
SOFIA Takeoff Audio
Stardust: Passing Comet Tempel 1
Voyager: Interstellar Plasma Sounds
Voyager: Lightning on Jupiter

M4R (iPhone):

Atlas V: Launch
Cassini: Enceladus Sound
Cassini: Saturn Radio Emissions #1
Cassini: Saturn Radio Emissions #2
Juno: Morse code “HI” received from Earth
Kepler: Star KIC12268220C Light Curve Waves to Sound
Kepler: Star KIC7671081B Light Curve Waves to Sound
LCROSS: Water on the Moon Song
Stardust: Passing Comet Tempel 1
Voyager: Interstellar Plasma Sounds
Voyager: Lightning on Jupiter

Beeps and Bytes
History changed on Oct. 4, 1957, when the Soviet Union successfully launched Sputnik from the Baikonur Cosmodrome in Kazakhstan. The world’s first artificial satellite was about the size of a beach ball, about 23 inches in diameter and weighing less than 190 pounds.
Here’s a collection of sounds from various missions. We have included both MP3 and M4R (iPhone) sound files to download. Note: M4R files must be downloaded and imported via iTunes. They will not play in your browser.
MP3:

Chorus Radio Waves within Earth’s Atmosphere

Courtesy of Electric and Magnetic Field Instrument Suite and Integrated Science (EMFISIS) team at the University of Iowa

Quindar: Sound #1
Quindar: Sound #2
Sputnik: Beep

M4R (iPhone):

Chorus Radio Waves within Earth’s Atmosphere

Courtesy of Electric and Magnetic Field Instrument Suite and Integrated Science (EMFISIS) team at the University of Iowa

Quindar: Sound #1
Quindar: Sound #2
Sputnik: Beep

Sounds of the Future