Experimental payloads for a manned Mars flyby mission
Experimental payloads for manned Mars flyby mission, including onboard remote sensors and unmanned probes for measuring Martian environment
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Experimental payloads for manned Mars flyby mission, including onboard remote sensors and unmanned probes for measuring Martian environment
Flyby infrared absorption measurements in Martian atmosphere for determination of profiles of carbon dioxide, particulate matter and water vapor
Science subsystems for Jupiter flyby missions, discussing equipment selection, mission planning, spacecraft design and trajectory and constraints on vehicle configuration
Navigation and guidance analysis of Mars probe launched from manned flyby spacecraft for 1975- 1976
Trajectory optimization, performance and other factors in analysis of low thrust solar electric propulsion Jupiter flyby mission
A first-order perturbation theory exists for the flyby problem with the Born approximation as the reference orbit.
none given - From Synopsis & Objectives: JPL has analyzed and developed for SDIO a preliminary mission design for a deep space mission to flyby two near Earth asteroids, Eros and Toutatis.
This paper describes the Casini orbit determination effort from injection through the first Venus flyby. Emphasis is placed on orbit determination modeling and the resulting orbit solutions.
Scientific exploration of Venus using an atmospheric probe requires relaying telemetry to Earth as the probe descends through the atmosphere to the surface of Venus. Using the flyby spacecraft to relay the probe telemetry to Earth will require precise carrier-to-probe pointing accuracy of the relay spacecraft’s antenna. NASA’s Deep Atmosphere Venus Investigation of Noble gases, Chemistry, and Imaging (DAVINCI) mission uses this carrier-to-probe relay technique. Although DAVINCI includes a coherent cross-link for science, this is not baselined for navigation tracking. This paper explores the potential effectiveness of cross-link tracking for reducing trajectory uncertainty and improving spacecraft-to-probe pointing.
Cosmological domain walls can be formed as a result of symmetry breaking at any epoch during the evolution of our universe. We study their interaction with a classical macroscopic object, like Earth or a satellite in Earth’s orbit. We set up an action that includes the interaction term between the massive classical object and the scalar field that the domain wall is made of. We use numerical calculations to solve the coupled equations of motion which describe the crossing between the domain wall and the classical object. Depending on the strength of the interaction, relative velocity and size, the object can be either stopped by the wall, or it can pass through it inducing deformations in the wall that cost energy. At the same time, the coupling to the scalar filed might change the object’s mass during the crossover. The fact that satellites in Earth’s orbit (or planets in Sun’s orbit) can change their mass and/or lose energy interacting with walls can be used as a new domain wall detection probe. For example, a typical velocity precision of a satellite is about 0.5 mm/s, which directly puts an upper limit on its mass change to ΔM/M ≲ 5 × 10 –17 . Alternatively, a known satellite flyby anomaly can easily be explained as an interaction with a closed domain wall. We also show that the presence of matter modifies the scalar filed potential and can locally create a bubble of the true vacuum, and thus trigger the decay of the false vacuum. For a critical bubble which is able to expand, such an interaction with the domain wall must be strong enough.
Dynamic effects are an important determinant of chemical reactivity and selectivity, but the deliberate manipulation of atomic motions during a chemical transformation is not straightforward. In this work, we demonstrate that extrinsic force exerted upon cyclobutanes by stretching pendant polymer chains influences product selectivity through force-imparted nonstatistical dynamic effects on the stepwise ring-opening reaction. The high product stereoselectivity is quantified by carbon-13 labeling and shown to depend on external force, reactant stereochemistry, and intermediate stability. Computational modeling and simulations show that, besides altering energy barriers, the mechanical force activates reactive intramolecular motions nonstatistically, setting up “flyby trajectories” that advance directly to product without isomerization excursions. A mechanistic model incorporating nonstatistical dynamic effects accounts for isomer-dependent mechanochemical stereoselectivity.
Noise characteristics of unified S-band tracking system high speed range rate and X-Y ANGULAR data obtained during aircraft flyby tests
Planetary atmospheric absorption spectroscopy employing split-trajectory dual flyby mode
Venus lander probe for manned flyby missions
Navigation and guidance analysis of Mars probe launched from manned flyby spacecraft
Assessing cryogenic fluid requirements and storage methods for manned earth orbital and Mars flyby missions, and parametric data on thermal protection schemes
Science subsystems for Jupiter flyby missions, discussing equipment selection, mission planning, spacecraft design and trajectory and constraints on vehicle configuration
Planetary atmospheric absorption spectroscopy employing split trajectory dual flyby mode