Girl Scouts of the Colonial Coast K-5 SmartFlower Curriculum
Solar Energy Curriculum for K-5 Girl Scouts
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Solar Energy Curriculum for K-5 Girl Scouts
Solar Energy Curriculum for 6th-12th grade Girl Scouts
A search is presented for narrow resonances, with a mass between 0.6 and 1.8 TeV, decaying to pairs of jets, in proton-proton collisions at $\sqrt{s}=13$ TeV. The search is performed using dijets that are reconstructed, selected, and recorded in a compact form by the high-level trigger in a technique referred to as “data scouting”, from data collected in 2016–2018 corresponding to an integrated luminosity of 117 fb −1 . The dijet mass spectra are well described by a smooth parameterization, and no significant evidence for the production of new particles is observed. Model-independent upper limits are presented on the product of the cross section, branching fraction, and acceptance for the individual cases of narrow quark-quark, quark-gluon, and gluon-gluon resonances, and are compared to the predictions from a variety of models of narrow dijet resonance production. The upper limit on the coupling of a dark matter mediator to quarks is presented as a function of the mediator mass. The sensitivity of this search goes beyond what is expected from statistical scaling with the integrated luminosity alone, as a consequence of the use of fewer parameters in the background function within a more robust statistical procedure.
Searches for pair-produced multijet signatures using data corresponding to an integrated luminosity of 128 fb - 1 of proton-proton collisions at s = 13 TeV are presented. A data scouting technique is employed to record events with low jet scalar transverse momentum sum values. The electroweak production of particles predicted in R -parity violating supersymmetric models is probed for the first time with fully hadronic final states. This is the first search for prompt hadronically decaying mass-degenerate higgsinos, and extends current exclusions on R -parity violating top squarks and gluinos.
Thermodynamic and physical properties of solid propellant for MARC 36Al spin rocket motor for Scout vehicles - static test firing of rocket motors
Low-density phenolic nylon charring ablator nose cones for Scout reentry project
Design feasibility of Scout launched recoverable lifting reentry vehicle test bed
Feasibility of Scout launched small lifting reentry vehicle for testing materials and thermostructures of full scale reentry vehicles
Vehicle instrumention and ground support equipment development to improve vertical and roll alignment of Scout launch vehicle
Error sources and their magnitudes in Scout launch vehicle data
Electrostatic potential sensors for use on NASA Scout vehicle S-131R
Modified BE-3 engine for fifth stage of Scout launch vehicle
Tabulated results of error analysis for reentry and escape missions of Scout launch vehicle
Rocket motor integration into Scout vehicle to improve performance
Scout missile destruct charge system premature operational response to high temperature environment caused by combustion gas leak during stage separation
Scout first stage jet vane effectiveness, and aerodynamic pitching and yawing moment coefficients determined from flight data
Effects of larger Scout D and B heat shields on vehicle stability and control, structure, and ground support equipment
Static aerodynamic characteristics of Scout fin with enlarged tip control at Mach numbers from 0.40 to 4.63