Microorganisms in the upper atmosphere emanate from surface and marine ecosystems (Burrows et al., 2009), and are capable of reaching high altitudes by strong uplifting forces or mixing between the troposphere and stratosphere (Homeyer et al., 2011; Randel and Jensen, 2013). In addition to microbes naturally lofted, landfills, wastewater treatment plants, slash-and-burn agriculture, air traffic, and desertification also contribute to the total amount of bioaerosols in the atmosphere (Smith, 2013). Prevailing winds can connect distant biomes on Earth (Creamean et al., 2013; Smith et al., 2013), and residence time in the upper atmosphere exerts a harsh combination of stresses on microbes outside the range of conditions normally encountered on the surface (e.g., lower pressure, higher irradiation, desiccation, and oxidation). Thus, airborne transport might provoke exceptional types of cellular damage or mutation. Some bacteria found in previous atmospheric surveys (reviewed by Griffin (2007) and Polymenakou (2012)) have traits that would improve persistence aloft – including cell pigmentation, DNA repair, and the ability to form endospores (hereafter referred to as ‘spores’). While microbial survival has been examined using environmental simulation chambers (Smith et al., 2011) and small meteorological balloons (Beck-Winchatz and Bramble, 2014), more comprehensive platforms for controlled, long-duration experiments in the upper atmosphere are needed. Earth's middle stratosphere, about 25 to 40 km above sea level (ASL), resembles the surface conditions of Mars (Kaplan, 1988); thus, the planetary protection community could obtain an improved understanding of the survival of terrestrial microbes on Mars rovers and landers by flying stratospheric experiments. Furthermore, data from survival experiments could contribute to models for bioaerosols carried on globally-circulated winds (Smith et al., 2013; Yu et al., 2013), which is vitally important to global food security (Brown and Hovmøller, 2002). For example, aerially-dispersed wheat fungi threaten a staple calorie and protein source for 4.5 billion people across 94 developing nations (Singh et al., 2011).
Studying microbial survival in the upper atmosphere presents two fundamental challenges: first, removing potential influences from pre-flight, ascent, descent, and landing so as to limit the experiment to targeted altitudes; second, maintaining aseptic conditions within a closed payload system to preserve the integrity of test samples. Large scientific balloons provide unique access to the stratosphere and careful control over exposure experiments. Our aim in this study was to design, construct, and fly a self-contained payload (autonomous avionics, power, environmental sensors) that could attach to the exterior of large balloon gondolas, permitting a survival-based microbiology experiment at desired altitudes. A secondary aim was to collect baseline data and establish microbiology procedures (including ground and negative controls) for enabling future science flights. We worked with
Exposing Microorganisms in the Stratosphere (E-MIST) was built to mount onto the exterior of a high-altitude balloon gondola (Figures 1–2). The payload (83.3 cm × 53.3 cm × 25.4 cm; mass 36 kg) had four independent “skewers” (Figure 3) that rotated 180° for exposing samples to the stratosphere. During ascent or descent, the samples remained enclosed within dark cylinders at ~25°C. Each skewer had an aluminum base plate holding ten separate, rectangular aluminum coupons (M4985, Seton) with spore samples deposited on the surface. Coupon dimensions were 5.40 cm (w) × 1.75 cm (h) × 0.51 cm (thick), including 0.28 cm diameter holes on ends for mounting to skewer base plates. The inside of each cylindrical skewer was a frame laced with Nomex felt to prevent outside light from leaking into the system. A hex shaft through each skewer was attached to a gear system powered by a commercially-purchased motor (SPG30E-300K, Cytron) controlled by a four-channel FD04A motor controller (Brushed DC Moto Controller, Cytron). The motors, gears, and light shield were held together by a frame composed of aluminum cutouts and 3D-printed polycarbonate-ABS components.
T-slotted 80/20 aluminum extrusions formed the framework of the E-MIST payload, with detachable, white powder-coated aluminum panels on each face of the box. Angle brackets on the back plate were used to mount the system onto the balloon gondola and four foldable handles (McMaster-Carr) were attached to the front-facing frame. Multiple sensors, instruments, and computers were embedded within the housing. In the center of the system was a stand-alone radiometer (PMA2100, Solar Light) with two ultraviolet (UV) sensors (PMA2107 and PMA2180, Solar Light) that measured UV levels (400 to 230 nm) every five min. The front panel data port contained two Universal Serial Bus (USB) ports, two light emitting diodes (LEDs), a Secure Digital (SD) card module, and two key switches. One key switch was used to power on the system and the other was used to manually rotate the skewers (for loading and removing samples). A sliding door on the front port assembly was held in place by two small magnets. One of the USB ports was used to start, stop, and retrieve data from the HOBO, a stand-alone external humidity and temperature sensor (U23-001, Onset) that collected data every ten s. The other USB port was used to retrieve data from the radiometer. LEDs illuminated when the global positioning system (GPS) (SPK-GPS-GS4O7A, S.P.K. Electronics Co.) had a lock on location (altitude, time, latitude, and longitude) and when the flight computer was on. The SD card (uDRIVE-uSD-G1, 4D Systems) module used a universal asynchronous receiver/transmitter to poll a microcontroller (Mega2560, Arduino) and the SD card.
Other major payload components included: an altimeter (MS5607, Parallax), three 8.5 W heaters, three resistance temperature detector (RTDs) (SA1-RTD-B, Omega), and a temperature and humidity sensor (RHT03/DHT22, Aosong Electronics Co.). Power was generated by a 14.8 v 25.2 Ah lithium-ion polymer battery (CU-J141, BatterySpace) fastened in place with a stainless steel battery holder. The power circuit used a DC-DC converter for stepping down 14.8v to 5v. Thermal performance for the payload during tropospheric ascent was modeled using Thermal Desktop (C&R Technologies). Heating pads (5V Heating Pad 5×10 cm, WireKinetics) were included in the payload so that in-flight heat pulses could keep sensors and instruments within desired operating temperature ranges. This regulation system was controlled by the flight computer and RTDs on the battery, radiometer, and sample base plate. An additional RTD was placed on a proxy coupon located on the front E-MIST panel.
Spore viability was measured using the Most Probable Number (MPN) enumeration technique that has been described elsewhere (Mancinelli and Klovstad, 2000; Smith et al., 2011). In brief, spores were dislodged from coupons by vortexing in sterile deionized water and sand for 2 min, and then processed through 6 consecutive serial dilutions. Using 96-well plates, 20 μl from each serial dilution, and 180 μl of sterile media (Per 1 L: 16 g Difco nutrient broth, 5 g KCl, 0.22 g CaCl2, 1.6 g FeCl3, 3.4 mg MnSO4, 12 mg MgSO4, 1 g D-glucose) were loaded into 16 wells per dilution and scored (presence or absence of bacterial growth, assessed by turbidity) after incubation for 36 h at 30°C.
We followed the ribonucleic acid (RNA) recovery procedure described by Moeller et al. (2012) to demonstrate the feasibility of this method with our flight coupons. Briefly, spores were lifted from coupons using a 1 ml polyvinyl alcohol solution. Air bubbles were removed by running a sterile glass slide coverslip across the polyvinyl alcohol aliquot, which was then dried overnight inside a petri dish and re-suspended in 1 ml of sterile molecular grade H2O. Next, spores were germinated using the protocol established by Nicholson et al. (2012), with each centrifugation step at 5,000 rpm for 10 min, except for the final culture volume that was spun down at 14,000 rpm for 5 min. Samples were processed with RNeasy® Protect Bacteria Kit (Cat. No. 74524, Qiagen Inc.) using protocols supplied by the manufacturer. Sample processing then continued at Step 3 Part 1 of the RNeasy® Mini Kit (Cat. No. 74104, Qiagen), followed by an on-column DNase digestion in Part 2 of the RNeasy® Mini Kit (Steps 1 to 4). Finally, the RNA cleanup in Part 2 of the RNeasy® Mini Kit (Steps 5 to 7) were followed, including the optional spin after Step 5 and elution in a volume of 30 μl RNase-free H2O. RNA yield was measured using the Qubit® 2.0 Fluorometer and standards from the Qubit® RNA HS Assay Kit (Cat. No. Q32855, Life Technologies).
A fully integrated test flight (all payload components powered on and
Temperature, relative humidity (RH), atmospheric pressure, and UV levels were measured across the test flight by our team and additional CSBF instruments. Each E-MIST skewer base plate carried 10
Our test flight demonstrated the functionality and reliability of a new payload for exposing microbes in the stratosphere. Baseline data collected can better prepare future research teams using this system. Table 1 summarizes upper and lower limits of key environmental data from the balloon launch, ascent, and float. Internal payload heaters performed nominally, keeping hardware components and sensors within operating limits – particularly in the upper troposphere during the coldest part of the flight. For instance, at 16.4 km ASL when the free air temperature was −67.5°C (measured by an independent, CSBF gondola sensor), the avionics board inside E-MIST remained at −4.10°C. However, a few instruments and components did not function properly. First, the altimeter failed, possibly due to radio frequency interference with other gondola instruments. Second, UV measurements were lost because the stand-alone radiometer was not powered off during payload recovery (forcing the instrument to eventually overwrite the data stored during float). Obtaining UV data on future experiments will be critical since other survival studies have shown a relationship between irradiation and bacterial inactivation (Smith et al., 2011). Looking forward, modifying the radiometer to store data on the payload flight computer will resolve this issue, and stratospheric UV measurements from other balloon missions (e.g., McPeters et al., 1984) can be used to establish an expected range of irradiation. Finally, the rotation of the sample skewers was suboptimal. In principle, end-to-end bacterial coupons will receive near-identical sunlight if the skewers open evenly (on the same plane) and no shadows cross the payload face – yet, neither condition was observed in flight. Intermittent gondola shadows passed over the skewers but were transitory since the balloon was constantly rotating. We will build a smart switch system that communicates with the motor controller to ensure skewers open evenly on the next flight opportunity.
Launch, Ascent, and Float Profile.
Atmospheric Pressure (mb) | 837 | 4.26 | Altitude of Ft. Sumner, NM, 1.25 km ASL |
Air Temp. (°C) | 23.3 | −67.5 | CSBF Free Air Thermistor |
Payload External Temp. (°C) | 18.5 | −13.7 | HOBO measurements |
Payload Internal Temp. (°C) | Internal heaters pulsed during acent and descent | ||
Avionics | 22.3 | −4.10 | |
Proxy Coupon | 46.1 | −28.0 | |
Battery | 16.0 | −4.65 | |
Radiometer | 37.1 | 4.15 | |
Payload Internal RH (%) | 65.0 | < 3.5 | Measurements below sensor sensitivity |
Payload External RH (%) | 60.5 | < 3.5 | Measurements below sensor sensitivity |
UV (W m−2) | N/A | N/A | Data were lost; see text for details |
Concerns about contamination (e.g., external microbes penetrating the payload) or inactivation (e.g., outside biocidal factors besides stratospheric conditions) motivated this methods-focused study. Including
Most Probable Number of Viable Spores.
Lab Ground Coupons | Kept in the laboratory | 1.84 × 106 (1, N/A) |
Transported Ground Coupons | Transported to launch site but not installed | 1.93 × 106 (2, 3.74 × 105) |
Face-Up Flight Coupons | Flown, exposed for 2 s | 1.91 × 106 (4, 4.30 × 105) |
Inverted Flight Coupons | Flown, exposed for 2 s without sunlight | 1.66 × 106 (4, 5.96 × 105) |
If future flights deployed the same experimental design and exposed microbes for hours at float, we would expect to see a rapid inactivation. Smith et al. (2011) simulated stratospheric conditions and measured a 99.9% loss of viable
Earth's stratosphere is extremely dry, cold, irradiated, and hypobaric, and it may be useful for the archive of microorganisms isolated from NASA spacecraft assembly facilities (e.g., Benardini III et al., 2014) to be evaluated in an environment analogous to Mars. Survival-based studies were recently deployed outside the International Space Station (ISS) (Horneck et al., 2012) and the same category of experiments can be conducted in the stratosphere. We hope the baseline data, procedures, and controls discussed herein can provide a pathway for future investigations using E-MIST. While spore-forming bacteria have remarkable resistance to atmospheric extremes, non-spore-forming bacteria, archaea, fungi, algae, and viruses should also be examined. A species-specific inactivation model that predicts the persistence of microbes in Earth's upper atmosphere (e.g., pathogenic cereal rusts), or even on the surface of Mars, is one of many possible outcomes from stratospheric microbiology research.