Progress report four for the On-Planet team for Friday March 03, 2000

 

For this week’s progress the On-Planet team continues the research required for experimentations to be conducted on the planet once the astronauts arrive.

 

1) Landing on the Surface

 

Landing Sites

 

Once the astronauts enter the atmosphere our main objective is where to land.  In our second progress report we chose several Martian landing sites that should be considered.  In total, according to NASA Reference Publication 1238, the Landing Site Catalog, there are approximately 153 possible landing sites.  For a list of these sites you may visit:

 

http://cmex-www.arc.nasa.gov/MarsTools/Mars_Cat/Mars_Cat.html

 

We propose to have a target-landing zone near the equator.  One good target zone is the place where the pathfinder landed, near the Ares Vallis region – a region scarred by ancient water channels.  Or the HEBES CHASMA site, which is excellent for analysis of soil because of the sediment, layered walls.

 

Surface Operations

 

Once there, the primary activities, of course, are the setup, organization and systems check of the surface equipment.  Mission Support should have a design whereby the habitat and laboratory modules can easily be attached together and powered by the nuclear power module.  The crew will then be able to conduct the previously planned experiments immediately after all equipment has been set up.  Since this is going to be about a 500-day mission, we have provided a list of vital Martian experiments to be conducted in our previous progress reports and later in this report.  The findings from these experiments will likely determine the direction of further investigations.

The geology and mineralogy of the surrounding area will be investigated and the search for evidence of life, either past or present, will continue.  Since this will be a two-crewed mission, each team will coordinate with each other and look for water in the Martian soil.  The crew will report their experiences on the surface of Mars back to mission control.  The crew will also have leisure and “vacation” time so that they can appreciate the experiences of being the first humans to walk on Mars.

 

2) More experiments involving on-planet experimentation

 

Nuclear Magnetic Resonance

 

            NMR studies the atoms or molecules with nuclear spins. From interactions with electrons and neighboring nuclei, NMR spectra of molecules show unique lineshapes or chemical shifts. This information can be used for characterization purposes. Also by completing NMR spectroscopy one can obtain information about the constituent nuclei and chemical structure of molecules. Specific applications of NMR on Mars include presence of water in the soil, minerals and rocks; free water in rock pores; absorbed water on surface; and chemically bound water.

            Also by utilizing proton-NMR, one can determine the quantity and physical and chemical nature of water (ex. H20, OH) in geological samples. Proton NMR is operated .1-1 g samples in an applied magnetic field by irradiation of radio frequency (~ 13 MHz at ~ 3 kGuass) to induce transitions between proton spin states.

 

INSTRUMENTS REQUIRED: miniature magnetic resonance spectrometer (< 500      

                 g, < 5 W) with combined capabilities of EPR and            

           NMR (being developed at JPL), a proton-NMR                      

spectrometer

 

X-RAY FLUORESCENCE ANALYSIS (XRF)

 

            This is a bulk chemical analysis method. Bulk chemistry of single mineral grains can provide important clues to their identity and in addition to other structural data identification is almost assured. One of these instruments, which was proposed for the Mars '98 missions, uses XRF primarily as a mineralogical tool. It analyzes powder samples in a transmitted, forward reflection geometry either as-received (wind-blown) or by grinding or drilling operations. This instrument yields bulk composition and X-ray diffraction data simultaneously.

INSTRUMENT REQUIRED: XRF instrument. Mass = 800 g, Power needed =

3 W       

                               Size = 11 x 11x X-ray source:                

                      Copper anode X-ray tube

 

SCANNING ELECTRON MICROSCOPE

 

            A scanning electron microscope with chemical analytical capability using energy dispersive analysis (SEM/EDX) could be useful in mineralogy as a source of morphological and compositional data on individual mineral grains.

 

RAMAN SPECTROSCOPY

 

            This is an optical scattering technique, which can provide molecular and

crystal-structural information about solid materials. Raman spectroscopy is an established laboratory method for identification and characterization of organic/hydrocarbon and inorganic/mineral substances. The spectral frequency shifts of Raman scattering are related to molecular structures in the same way as the absorption/emission transitions in infrared absorption, reflectance, and emission spectroscopy. Many of the problems in interpreting infrared spectra (ex. size effects, transparency peaks, volume scattering) are not problems in Raman Spectroscopy. Also Raman spectra can readily distinguish crystalline and glassy materials.  Some downfalls of this technique are that long analysis times are required, high-power light sources, and a large power flux is required. Also once a Raman spectrum is obtained, it is not clear how well spectra of mineral mixtures can be deconvolved to yield species or the abundance of the constituent minerals; and what the minimum detectable mineral abundance is. The answer could lie in the technique of microscopic Raman spectroscopy on single mineral grains (a standard laboratory technique).

INSTRUMENTS NEEDED: a microscopic Raman spectroscopy instrument

 

OPTICAL LUMINESCENCE SPECTROSCOPY

 

            Optical luminescence is emission of non-thermal optical photons as a response to energy input. Fluorescence is prompt emission in response to high-energy photons, and can be useful in determinative mineralogy, especially of ionic salts (carbonates, sulfates). Fluorescence can arise from essential elements (or ions), trace element substituents (activators), or defects. Optical luminescence may be useful for surface investigation on Mars, as atmosphere surface interactions may have produced ionic salts of the alkali and alkaline earth elements. Many common minerals that do not luminesce at visible wavelengths may do so in the infrared. Nonetheless there are some limitations, such as it cannot provide mineral proportions or compositions, and there has been little systematic investigation of luminescence at infrared wavelengths or faint luminescences.

 

INSTRUMENTS NEEDED: a vis-NIR spectrometer, short-wavelength light          

           source

 

THERMAL ANALYSES

 

            Many minerals transform or react during heating, and the thermal effects of those transformations can be characteristic of particular minerals. There are two standard methods, the differential thermal analysis (DTA) and differential scanning calorimetry (DSC). In both of these methods the unknown sample is introduced into a heating chamber in close proximity to a reference sample and they are heated. In DTA, the sample and reference are heated at a constant rate and in DSC sample and unknown are heated separately so that both stay at the same temperature. Currently, DSC is limited to thermal effects below 700oC and DTA is limited to temperatures below 1200oC. By itself thermal analysis can detect the heat effects associated with crystalline phase changes, magnetic order/disorder transition, chemical reactions, and melting. Coupling thermal analysis techniques with the method of analyzing gasses evolved during heating are especially helpful. Such gas analyzing techniques could be by the mass spectrometer and by gas chromatography. This combination of methods can provide info about the mixtures and complex soil samples in the unknown sample. Thermal/evolved-gas methods are particularly powerful for volatile-rich materials. Also it becomes easier to distinguish among clays, silicates, feldspars, zeolites, glasses, and evaporites.

 

NEEDED INSTRUMENTS: a thermal analysis instrument (don't know if any        

              are flight qualified) Ex. Gooding et al instrument            

         (TAPS)---has DSCs with evolved gas analysis by compound-specific sensors.  Mass = 1 kg, Energy = 5 W-hr per analysis of a 20-50 mg sample

 

MAGNETIZATION

 

            A result from the Viking missions was the discovery that the Martian soil is highly magnetic because the soil was attracted by a small permanent magnet. Magnets brought up to Mars for future missions should be of lower strengths than the weakest Viking magnets. The magnets should be completely immersed in a thin magnesium plate. The magnets would be of equal strength, but mounted at different depths below the surface of the magnesium plate. Discrete (single phase) particles of the strongly magnetic minerals will stick to the weaker magnets, while composite (multiphase) particles will stick only to the strongest magnets. The Magnet Array may be able to perform X-ray fluorescence and Mössbauer analysis of the dust on the magnets.

NEEDED INSTRUMENTS: The magnetic array could contain 5 magnets of different strenths. Mass = 70 g, Outer Diameter of  Magnets = 18 mm each

 

 

3) More experiments involving human physiology

 

Renal Stone Risk Assessment

 

Goal:

(1) To determine the effects of exposure to microgravity on the potential for renal stone formation.
(2) To determine the effect of mission duration on the potential risk for renal stone formation.
(3) To determine how long after flight the increased risk exists for renal stone formation.

 

Approach:

The three crewmembers collected urine voids over a 24-hour period three times during the preflight period (L-148, L-58 and L-34), and following landing on R+0, R+6, R+10 and R+13. Inflight urine samples were collected on Mission Day (MD) 14, MD 93 and MD 110. Inflight, individual urine voids were collected into a urine collection device containing 1 ml lithium chloride as a volume marker. Two 7 ml urine aliquots were drawn into syringe tubes containing 0.05% thymol or 0.1% thimerosal, mixed well and stored at ambient temperatures until return to Earth for analyses. Following the return of the samples, urine volumes were determined from the diluted lithium concentration. Twenty-four-hour urine pools were constructed from the individual voids and samples were analyzed for osmolality, calcium, oxalate, uric acid, citrate, sodium, sulfate, phosphorus, magnesium, potassium and creatinine.

Pre- and postflight, the subjects collected 24-hour urine specimens. The pooled urine was stored chilled at approximately 4 degrees Celsius. After total volume and pH were recorded, two 10 ml aliquots were removed for biochemical analysis. The first sample was analyzed for creatinine, magnesium, phosphorus, potassium, sodium and uric acid. The second 10 ml aliquot was acidified with 6M hydrochloric acid (HCl) and analyzed for calcium, magnesium, citrate, oxalate and sulfate. All samples were processed immediately or stored at -20 degrees Celsius until analysis.

From the measurements, the relative urinary supersaturation of the stone forming salts were calculated and renal stone risk was estimated. The derived parameters were urinary supersaturation of calcium oxalate, brushite (calcium phosphate), sodium urate, struvite (magnesium ammonium phosphate) and uric acid saturation.

 

Somatic Embryogenesis of Orchardgrass in Microgravity

 

Goal:

The overall objective of this research was to provide information on the influence of microgravity on embryo initiation, differentiation and development and the ultimate reproductive capacity of resultant plants, using an in vitro culture system in orchardgrass (Dactylis glomerata L.) in which the target cells remain in situ. The system was based on paired half-leaf segments, which provided a precise control and the opportunity to use paired statistics for analyses of the data.

 

Approach:

Somatic embryos form directly from mesophyll cells in cultured leaf segments and develop fully to a germinable stage. The basal 3 cm of the youngest two leaves were split down the midvein. Beginning at the base, these were cut transversely into six segments approximately 3 mm square. Segments from one half-leaf were used for the flight treatments and the corresponding sister segments served as controls. This provided a precise control for each treated leaf segment and the opportunity to use paired statistics for data analysis . Observations and data were collected on quality and quantity of embryo formation, axis determination and polarity. Embryo number was estimated using an already-developed formula and extensive histological data. Plants were established from somatic embryos and used for mitotic chromosome analyses. The same plants were transferred to the field and used for meiotic chromosome analyses and estimation of pollen fertility.

 

Hardware:

Biological Research In Canisters (BRIC-100)

Developmental and Physiological Processes Influencing Seed Production in Microgravity

 

Goal:

The investigator hypothesized that a plant may become limited in gas exchange due to the lack of convective air movement in microgravity. Since plants depend on convective air movement to aid the uptake of metabolically important gases, the lack of convection may affect these processes. Since the CHROMEX-03 plants were carbohydrate-poor, carbon dioxide transport to the plants may have been limited.

 

Approach:

Two Plant Growth Chambers (PGC) were used in the Plant Growth Unit, positions 3 and 4. Each chamber held 6 mouse-ear cress (Arabidopsis thaliana) plants, which were 14 days old at launch. The foam/agar plug nutrient system was used. A Warburg solution was added to the chamber to maintain carbon dioxide levels. The plants were flown for 10 days, and then recovered from the Shuttle for analysis. Measurements of pollen viability were made immediately after landing, and material was fixed for subsequent microscopy.

 

Hardware:

Plant Growth Mediums
Plant Growth Unit (PGU)

Changes in Total Body Water During Spaceflight

 

Goal:

Measure the changes in total body water (TBW) occurring in humans as a consequence of exposure to microgravity.

 

Approach:

TBW was measured by the isotope dilution technique using a dose of approximately 6 g of [18]oxygen-labeled water (H[2][18]O) as the tracer. After ingestion of the tracer, saliva samples were collected on dental cotton rolls over a period of several hours. Inflight and postflight data were compared to preflight (baseline) data. Body mass was measured before and after flight, to enable calculation of the TBW to total body mass ratio. Data were analyzed according to the general mixed model analysis of variance.

 

Hardware:

Drink Container
Saliva Collection Kit
Tracer Kit

Gravity and Skeletal Growth: III. Recovery of Osteogenic Potential

 

Goal:

Data from previous space flight missions suggest an initial inhibition of osteoblast histogenesis followed by a postflight recovery response. This study of rat maxillary molar periodontal ligament (PDL) allowed further investigation of the osteoblast histogenesis recovery pattern.

 

Approach:

Samples were demineralized, embedded in plastic, sectioned (4 µm) in the mid-sagittal plane of the medial root of the first molar, and stained with hematoxylin and eosin. An ocular micrometer was used to measure the major and minor nuclear dimensions of 100 cells in each PDL under oil immersion at 1,000x. Nuclear volume for each cell sampled was calculated according to the formula for a prolate spheroid. The fractional distribution of each cell type was expressed as group mean ±SEM. PDL width was also measured at three levels within the mid-root region of the medial root of the first molar.

 

4) More hardware requirements

 

Microscopy StationThe Microscopy Station will study particle morphology, hardness, adhesion, and abrasion. The Microscopy Station consists of an Optical Microscope, an Atomic Force Microscope (AFM), and the Sample Delivery System. Combined, the Optical Microscope and AFM will enable the IIT IPRO team to image particles from millimeters to nanometers in size.

A series of soil samples from different depths below the surface will be, hardness test coupons, soft metals, "sticky" surfaces (polymer or textured), wear test coupons (e.g., visor material the adhesive and abrasive properties of the dust and soil on relevant materials.

Microscopy Station Diagram

Components of the IIT IPRO Microscopy Station

The Sample Delivery System consists of a rotary/linear drive and a sample wheel. It will present to the microscopes a series of dust samples on a variety of substrates. It will also position the substrates relative to a fixed multipurpose blade for removing excess material, and an abrasion tool for abrading selected substrates. The configuration of the system has been chosen to minimize the number of mechanisms required while still allowing soil and dust with the greatest range of properties to be successfully imaged.

The Sample Delivery System is from Surface/Interface, Inc

The Optical Microscope consists of an illumination system of superbright LEDs, an optical system, and a black-and-white CCD camera. Illumination will be provided in four colors (red, green, blue, and ultraviolet).

 

 

The Atomic Force Microscope is an outgrowth of the scanning tunneling microscope. The AFM measures atomic-scale forces between a surface and a probe tip by deflection of a microcantilever. The AFM produces topographic images of the surface with sub-angstrom resolution. MECA's AFM incorporates a miniature low-voltage electromagnetic drive element, piezoresistive sense elements, an array of scan probes, and autoimaging control software. The entire AFM head has been designed for mounting between the optical microscope objective lens and the sample with minimal compromise of optical imaging performance.

 

 

 

 


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