Isolation of Seismic Signal from InSight/SEIS-SP Microseismometer Measurements

The InSight mission is due to launch in May 2018, carrying a payload of novel instruments designed and tested to probe the interior of Mars whilst deployed directly on the Martian regolith and partially isolated from the Martian environment by the Wind and Thermal Shield. Central to this payload is the seismometry package SEIS consisting of two seismometers, which is supported by a suite of environmental/meteorological sensors (Temperature and Wind Sensor for InSight TWINS; and Auxiliary Payload Sensor Suite APSS). In this work, an optimal estimations inversion scheme which aims to decorrelate the short-period seismometer (SEIS-SP) signal due to seismic activity alone from the environmental signal and random noise is detailed, and tested on both simulated and Viking data. This scheme also applies a module to identify measurements contaminated by Single Event Phenomena (SEP). This scheme will be deployed as the pre-processing pipeline for all SEIS-SP data prior to release to the scientific community for analysis.     

Topside sounding of the earth's ionosphere

The evolution of topside sounding through rocket and satellite experiments is reviewed. Topside sounding has proved valuable for revealing the structure of the high ionosphere and for investigating the resonance properties of a magnetoplasma. The limits of our present knowledge of these rapidly developing subjects are discussed. Topside sounding is predicted to have a long and useful role in exploration of the ionosphere of earth and other planets.     

Ultraviolet emissions from the upper atmospheres of the planets

A large number of atoms and molecules have strong emission lines in the vacuum ultraviolet. As a result, this spectral region is particularly suited to studying the upper atmospheres of the planets. The observed emissions not only identify the constituents, but also provide information on the solar and magnetospheric excitation processes. Long term monitoring of these emissions, particularly with modest spatial resolution, can elucidate the effects of variations in the solar input as well as changes in magnetospheric conditions. Also, earth orbiting telescopes generally provide better spectral resolution than is available on flyby vehicles. A modest beginning in planetary upper atmospheric studies from earth orbit has been made using orbiting observatories designed primarily for stellar astronomy. As examples of the power of this technique, some recent results will be reviewed with an emphasis on Jupiter and the Io torus. The unusual scheduling requirements and the effects of scattered intense long wavelength radiation put demands on orbiting planetary observatories which are somewhat different from those of stellar astronomy. The implications of these demands for continued advances in this area are discussed.     

A Review of Hypervelocity Debris Testing at the Air Force Research Laboratory

In this paper, we describe a compact, low cost, fast turn-around-time technique used at the Air Force Research Laboratory to study hypervelocity debris impact effects on spacecraft structures and components. The technique described was used to study debris effects in the areas of: shock physics, debris-produced contamination, chemical analyses of the impact ejecta and debris initiated spacecraft discharge. Examples of research results obtained with the technique are presented and illustrate problems encountered in the field of space debris effects on spacecraft.     

A wave model for dwarf novae

The rapid coherent oscillation during a dwarf nova outburst is attributed to an accretion-driven wave going around the white dwarf component of the binary system. The increase and decrease in the period of this oscillation is due to the change in the velocity of the wave as it is first being driven and then damped. Qualitatively, a large number of observations can be explained with such a model. The beginnings of a mathematical representation of this model are developed.     

Simplified parametric cost trade-offs in satellite system design

In this paper, a parametric cost model for the space segment of a meteorological satellite system is derived and exercised to provide insight into the major economic trade-offs affecting the choice of the satellite's design life and replacement strategy. Trade-offs involving replacement strategy include launch via an expendable booster versus launch via the Space Shuttle; and recovery, repair, and reuse of a failed satellite versus simple replacement with no reuse.

The sensitivities of space segment costs to design life, launch costs, replacement costs, and refurbishment costs are examined with explicit inclusion of nonrecurring and recurring costs.

The results from an application of the model indicate that routine spacecraft retrieval and reuse of a modestly expensive spacecraft is not a significant economic benefit and that design lifetimes of three or four years are the best choice.     

Nitric oxide density enhancements due to solar flares

A differential emission measure technique is used to determine flare spectra using solar observations from the soft X-ray instruments aboard the Thermosphere Ionosphere Mesosphere Energetics Dynamics and Solar Radiation and Climate Experiment satellites. We examine the effect of the solar flare soft X-ray energy input on the nitric oxide (NO) density in the lower thermosphere. The retrieved spectrum of the 28 October 2003 X18 flare is input to a photochemical thermospheric NO model to calculate the predicted flare NO enhancements. Model results are compared to Student Nitric Oxide Explorer Ultraviolet Spectrometer observations of this flare. We present results of this comparison and show that the model and data are in agreement. In addition, the NO density enhancements due to several flares are studied. We present results that show large solar flares can deposit the same amount of 0.1–2 and 0.1–7 nm energy to the thermosphere during a relatively short time as the Sun normally deposits in one day. The NO column density nearly doubles when the daily integrated energy above 5 J m⁻² is doubled.     

在示波器校准中是否使用有源探头

测试工作的目标是把校准波形忠实地传送到被测示波器的输入端。多年来,人们已经开发了各种传送的方法来克服ＶＳＷＲ和其它的误差来源,其中一些方法较之其它方法更加实用,经济。概括介绍了一系列的实验并通过这些实验,我们对传统的的、比较复杂的使用脉部有源探头的方法和更加实用的同轴电缆的方法用示波器进行校准的情况做了比较。