Birds, housing, and flight training
Energy expenditure during flight was measured in Rose Coloured Starlings. This is a migratory species with its breeding grounds stretching from the Balkans throughout Central Asia and wintering on the Indian subcontinent. During their seasonal migration, Rose Coloured Starlings cover about 5,000 km mainly in diurnal flights (Hudde 1993). We exploited their willingness to perform long flights of several hours during the migration periods, and measured energy expenditure during these flights with the DLW method during March–May 2001, October–December 2001, and March–May 2002.
We measured flight costs in 14 individuals. Four of these birds were purchased in 1999 as nestlings from a breeder and flown in U flights (see below) in 2001 (Engel et al. 2006a), and 10 birds were collected as nestlings from a breeding colony on the Crimea peninsula, Ukraine, in 2001, performing U flights in autumn 2001 and C and L flights (see below) in 2002. All Rose Coloured Starlings were hand raised at our institute and thus were familiar with close presence of humans and handling. The juvenile birds from the Ukraine were regularly trained to fly in the wind tunnel during 8 weeks before the first experimental flights. Adult birds had been flying in the wind tunnel before. They were trained for 3 weeks before the experimental flights in autumn 2001 and for 5 weeks in spring 2002. During training flights, as well as during the experiments, birds flew in groups of 2 to 3, as the Rose Coloured Starling is a flock-living and also flock-migrating species, and the birds seemed to be more at ease in small groups than alone. However, they did not fly in any specific formation and changed their relative position in the wind tunnel frequently. During the weeks before an experimental flight, each bird had performed training flights of at least 90 min duration. All birds used in the experiment were in excellent condition without having any defects in their flight feathers.
The birds were housed in groups of 3–5 in aviaries adjacent to the wind tunnel (ca. 1 m × 2 m × 2 m). They received standard food, consisting of insects, beef heart, curd, rusk, and egg ad libitum supplemented with minerals and vitamins, some live mealworms and fresh fruit and salad. They had unlimited access to fresh water and the opportunity to bathe. The light schedule followed the conditions the birds would experience in the field: during winter, day length (from civil dawn to civil dusk) corresponded to the photoperiod of the wintering quarters in northern India (27.5°N). During spring, it increased weekly until it met the natural day length at 47.5°N in summer, matching the light conditions at the natural breeding grounds as well as at our institute. During autumn, we gradually changed the day length back to the conditions at the wintering grounds. To approximate the spectral composition of natural sunlight, we used Osram Biolux® lamps.
Experimental flights
Fourteen Rose Coloured Starlings flew repeatedly (up to 9 times) in the wind tunnel of the Max Planck Institute for Ornithology, Seewiesen, Germany (Engel et al. 2006a). Between the flights, body mass of the birds varied spontaneously between 56.1 and 89.9 g. Within individuals, variation in body mass (maximum-minimum) ranged from 2 to 30% of the minimum body mass (Fig. 1). During the experimental flights, birds flew either unrestrained (U), carried a control harness (C), which was applied immediately before the flight, or a loaded harness (L), which was applied either immediately before the flight (LS) or at least 9 days before the experimental flight (LL; see below).
For individuals, the time interval between flights was on average 12.7 ± 6.8 days with a minimum interval of 5 days. The loaded harnesses increased the mass of the birds by 7.4 ± 0.8% of the bird’s body mass (with 7.5 ± 0.9% in LS and 7.2 ± 0.5% in LL flights). This artificial load of 7.4% was applied because a pilot phase had revealed that birds could immediately and sustainably fly with these loads but not with loads of 20% of the bird’s body mass. To control for a potential increase in drag caused by the backpack birds in C flights were equipped with a very light harness, weighing on average 1.2 ± 0.1% of the bird’s body mass (ranging from 0.9 to 1.0 g) and similar in volume and shape to the fully loaded harness. The construction of the harness was based on the thigh-method described in Rappole and Tipton (1991; Fig. 2). The harness was flat, had an even surface, and rested on the bird’s lower back, the synsachrum. The additional mass was thus placed at the center of gravity, comparable to natural fuel loads. Feathers covered the anterior part of the harness and the loops. Because the harness was fixed at the bird’s thighs, without loops around the neck or wings as in other studies (e.g. Gessaman et al. 1991; Godfrey 1970; Goldspink 1977; Higuchi et al. 1996; Nicholls and Warner 1968), the birds did not run the risk of dying from oesophageal blockage (Pekins 1996) and their flight ability was not impaired.
As in the training flights, birds flew in groups of 2 or 3 during experimental flights. Although they could land in the wind tunnel, even while the wind was switched on, an observer standing next to the flight section during the whole flight prevented the birds from landing or leaving the wind tunnel by waving at them when necessary. The mere presence of this person was usually sufficient. The birds were observed during the whole flight. When a bird landed frequently or refused to start again, we let it rest for at least 15 min or took it out of the experiment.
Flight speed was constant within all flights. In U flights, flight speed varied between the flights, with an average equivalent air speed of 11.2 ± 1.5 ms−1 (SD 0.03 ms−1 within a flight, calculated from the internal data acquisition of the wind tunnel, sampling at a frequency of 1 Hz). For all other flights, flight speed was adjusted to 11.0 ± 0.0 ms−1. During the flights, birds covered on average 232.4 ± 28.3 km. Air temperature was set to 14.5 ± 0.5°C. The air pressure and relative humidity were not regulated (937.9 ± 8.9 mbar and 58.3 ± 10.3%, respectively).
Energy expenditure during flight, ef, and water flux
Energy expenditure during flight, ef, was measured with the Doubly Labelled Water (DLW) method (Lifson and McClintock 1966; Speakman 1997). The accuracy of DLW measurements increases when birds are in a postabsorptive state, as they switch faster from carbohydrate to fat combustion (Rothe et al. 1987). Hence, birds were food-deprived since the evening before the experimental flight in most of the measurements. For 8 of the U flights, birds had access to food in the morning before the experiment for about 60–90 min (Engel et al. 2006a). In the morning, shortly after lights on, we took a blood sample of about 60 μl to determine the background concentration of 18O and 2H in the experimental bird. Afterwards, the bird was injected intraperitoneally with about 0.2 g of a DLW mixture (enriched in 18O by 59.3 atom percent, and in 2H by 34.5 atom percent). The injected dose was quantitatively determined by weighing the syringe on an analytical balance (Sartorius® BP1215) to the nearest 0.1 mg. After the injection, the bird was placed in a dark box without access to food or water for 1 hour. We then took another blood sample of 60 μl (initial sample) from the jugular or the wing vein. From the dilution of the labelled isotopes with the body water pool, we calculated the bird’s total body water before the experimental flight (TBWinitial, in g). We took into account that calculations based on the isotope dilution method tend to overestimate TBW by 1.8% (Speakman et al. 2001). In treatment C and LS, we applied the harness after the blood sample and immediately before the flight. After the flight, 6.0 ± 0.49 h after the initial sample, the “final sample” of 60 μl was taken. Thereafter, we removed the harness in all treatments (C, LS, and LL). We injected the bird with 0.11 g DLW afterwards, which was weighed to the nearest 0.1 mg. After one hour of rest in the dark box, we took another blood sample (reinjection sample) before the bird was released in its aviary, where it had access to food and water again.
The reinjection sample allowed us to calculate TBW at the end of an experimental flight (TBWfinal), calculate exactly the water influx (rH2Oin, in g day−1) and water efflux (rH2Oout, in g day−1) and thus increase the accuracy of the DLW measurement. We related both TBW and rH2O to body mass (TBW%initial, TBW%final (in %), and rH2Oin and rH2Oout (in g kg−1day−1), respectively) to account for possible differences in body size. The bird’s body mass (m in g) was determined to the nearest 0.01 g on a Sartorius® BL 1500S balance immediately before and after the flight. In the following, we always refer to the average body mass during flight.
All blood samples were subdivided over four capillary tubes, immediately flame-sealed, and stored at 5°C for the isotope analysis. The isotope analyses were performed in triplicate or quadruplicate at the Centre for Isotope Research according to the method described by Visser et al. (2000). Briefly, for each sample 2H/1H and 18O/16O isotope ratios were determined with the CO2 equilibration method and the uranium reduction methods, respectively (Speakman 1997). The coefficients of variation for 18O and 2H enrichments relative to the background levels were 1 and 0.75%, respectively. Rates of CO2 production were calculated as described by Engel et al. (2006a). As a last step, these values were converted to energy expenditure using a conversion factor of 27.8 kJ l−1 (Gessaman and Nagy 1988a; Engel et al. 2006b), assuming that 4% of the energy is derived from protein breakdown and the rest from fat. This fuel composition is in the range of empirical estimates for migrating birds (Jenni and Jenni-Eiermann 1998; Klaassen et al. 2000; Battley et al. 2001). Assuming the unlikely case that 10% of the energy is derived from protein breakdown would lead to an increase of CO2 production by 2%. On average, the turnover rate of 18O was 3.11 (SD 0.634) times higher than that for 2H. Consequently, an analytical error of 1% in the measured isotope values would result in an error of about 4% in the calculated energy expenditure.
As the DLW method integrates over the energy spent between the initial and the final blood sample, we corrected for the energy expenditure during non-flight, i.e. for resting and handling periods, with the mass-specific metabolic rate of 0.021 W g−1 measured in postabsortive Rose Coloured Starlings during daytime at ambient temperatures above 12.9°C by Engel (2005) to yield the flight costs, ef (in W).
Breast muscle index and Wing beat frequency (WBF)
We assessed the “breast muscle index” before and after each flight by measuring the elevation of the muscle relative to the sternum at a standardized location to the nearest 0.01 mm with callipers (Fig. 3). This is a relative measure of muscle thickness. The first measurement of the breast muscle index was taken before the injection with DLW (henceforth referred to as initial breast muscle index), i.e. on average about 7.5 h before the last measurement after the flight. Three measurements were taken at each sampling time and averaged for further analysis. We measured the breast muscle index in the experimental birds of group C, LS, and LL. As a control for non-flight, we also measured it in 8 resting birds, which were kept under the same conditions except for the flight. The resting birds were measured in the morning and after about 7.9 h, a time span comparable to that in the flying birds. During that time, the birds were kept without access to food and water, and, as in the experimental birds, three blood samples were taken. Body mass of these resting birds was on average 90.4 ± 6.9 g during the measurement period.
WBF (in Hz) was visually analysed from video recordings of the flight (watec WAT−902H with 25 frames s−1). For a subsample of flights of treatments C (N = 12), LS (N = 12), and LL (N = 6), we analysed flight sequences of 10 s duration and averaged over five such sequences as former analyses had revealed that WBF did not detectably change during flight (Engel et al. 2006a; Schmidt-Wellenburg et al. 2007). We evaluated the “effective” wing beat frequency, i.e. we allowed for periods of bounding and gliding flight.
Statistics
The statistical analyses were performed in SPSS 13.0. The tests were two-tailed, and significance was accepted at P < 0.05. Data reported are averages ± SD (between flights). To account for repeated measurements, we tested for effects of body mass m (in g) on ef (in W) in linear mixed models with Restricted Maximum Likelihood (REML). Treatment (U, C, L, LS, and LL) was introduced to the analysis as a category, as the mass of the harness was correlated with m. The dependent variable was log10(ef); individuals were included as random, and log10(m), treatment, treatment × log10(m), and log10(WBF) as fixed factors. The interaction term and log10(WBF) were excluded from the models in a stepwise manner, if they did not significantly contribute to the explained variance.
We tested for effects of the total mass transported in a flight m
transp (in g), i.e. m plus the mass of the harness, on ef in linear mixed models with REML as described above. As flight speed was shown to not significantly affect ef in the U flights (Engel et al. 2006a), it was not included into the models. The effects of treatment and body mass on log10(WBF) were tested in a separate linear mixed model, analogous to the model described above.