A retrospective evaluation of the impact of a dedicated obstetric and neonatal transport service on transport times within an urban setting

OBJECTIVE:To determine whether the establishment of a dedicated obstetric and neonatal flying squad resulted in improved performance within the setting of a major metropolitan area.DESIGN AND SETTING:The Cape Town metropolitan service of the Emergency Medical Services was selected for a retrospective review of the transit times for the newly implemented Flying Squad programme. Data were imported from the Computer Aided Dispatch programme. Dispatch, Response, Mean Transit and Total Pre-hospital times relating to the obstetric and neonatal incidents was analysed for 2005 and 2008. RESULTS: There was a significant improvement between 2005 and 2008 in all incidents evaluated. Flying Squad dispatch performance improved from 11.7% to 46.6% of all incidents dispatched within 4 min (p < 0.0001). Response time performance at the 15-min threshold did not demonstrate a statistically significant improvement (p = 0.4), although the improvement in the 30-min performance category was statistically significant in both maternity and neonatal incidents. Maternity incidents displayed the greatest improvement with the 30-min performance increasing from 30.3% to 72.9%. The analysis of the mean transit times demonstrated that neonatal transfers displayed the longest status time in all but one of the categories. Even so, the introduction of the Flying Squad programme resulted in a reduction in a total pre-hospital time from 177 to 128 min. CONCLUSION: The introduction of the Flying Squad programme has resulted in significant improvement in the transit times of both neonatal and obstetric patients. In spite of the severe resource constraints facing developing nations, the model employed offers significant gains

Optimal Cross-Wind Towing and Power Generation with Tethered Kites

Non-powered flight vehicles such as kites can provide a means of transmitting wind energy from higher altitudes to the ground via tethers. Although there have been many proposals for systems to extract wind energy from higher altitudes, this paper focuses on the use of a light lifting body at the end of a tether to generate useful power. Two major configurations are studied: 1) the kite is used to tow a ground vehicle in the cross-wind direction, 2) the kite is flown to generate power using a ground generator. In both cases, the useful work done by the kite is transmitted to the ground through the tether. Both applications require automatic control of the kite. A simplified system model is used to study the nature of the optimal trajectories of the system for different wind speeds. Numerical results illustrate that optimal power generation requires complex three-dimensional kite trajectories, whereas cross-wind towing requires much simpler trajectories. A feedback tracking controller is demonstrated for tracking the kite trajectories in the presence of unsteady winds

The widths of the 9.991-MeV and 10.165-MeV levels in 27Al

Gamma radiation from the decay of two resonances in the reaction 26Mg(p, γ)27Al at Ep = 1.785 MeV and 1.965-MeV, have been resonantly absorbed in aluminium to excite the states at 9.991 MeV and 10.165 MeV, respectively. In addition the γ-decay of the resonances have been studied in detail and angular distribution and yield measurements of the ground-state radiation performed. The following results were obtained: 9.991-MeV Level 10.165-Mev Level Jπ 7 2(-) 5 2+ Γt 1.2 ± 0.3 eV 23 ± 3 eV Γp 0.5 ± 0.2 eV 22 ± 3 eV Γγ 0.7 ± 0.2 eV 1 ± 5 eV. The spin of the 9.629-MeV state in 27Al, excited at Ep = 1.409 MeV, was also determined and found to be 1 2. © 1968.Articl

The widths of the 9.991-MeV and 10.165-MeV levels in 27Al

Gamma radiation from the decay of two resonances in the reaction 26Mg(p, γ)27Al at Ep = 1.785 MeV and 1.965-MeV, have been resonantly absorbed in aluminium to excite the states at 9.991 MeV and 10.165 MeV, respectively. In addition the γ-decay of the resonances have been studied in detail and angular distribution and yield measurements of the ground-state radiation performed. The following results were obtained: 9.991-MeV Level 10.165-Mev Level Jπ 7 2(-) 5 2+ Γt 1.2 ± 0.3 eV 23 ± 3 eV Γp 0.5 ± 0.2 eV 22 ± 3 eV Γγ 0.7 ± 0.2 eV 1 ± 5 eV. The spin of the 9.629-MeV state in 27Al, excited at Ep = 1.409 MeV, was also determined and found to be 1 2. © 1968.Articl

Lifetime measurements on 26Mg and 29Si by Doppler shift attenuation

The lifetimes of the lowest bound states of 26Mg and 29Si were determined by means of Doppler shift attenuation measurements. The results are τm = 300+100-60 95±25, &gt; 5000and 2100+4000-1000fs for 26Mg (1) through (4) and τm = 560±130, 830±260 and 24±14 fs for 29Si (1) through (3), respectively. © 1970.Articl