Steering Towards Low-Carbon Road Freight Transport Through Policies - The Case of Oslo

The primary purpose of this thesis is to assess policy measures promoting the uptake and use of low-carbon technologies in urban road freight transport (URFT) in Oslo, Norway. This sector has historically received little attention compared to passenger and public transport, but contribute to significant greenhouse gas (GHG) emissions, noise, and other negative health effects. Low-carbon vehicles in this research are referred to as electric and hydrogen vehicles, which could help mitigate these effects. To promote their uptake and use, policy measures must be implemented and synchronized with expectations from various stakeholders directly and indirectly impacting URFT. This is important to ensure effective results. Findings were collected through a literature review and semi-structured interviews with, among others, authorities, freight operators, original equipment manufacturers (OEM’s), and research organisations. Findings suggest several policy measures are needed to promote the uptake and use of low-carbon freight vehicles, most urgently in the category of fiscal measures, and facilitation of low-carbon infrastructure. Also, toll roads, fuel taxes and various subsidy schemes were stressed as necessary to reduce high costs for low-carbon URFT vehicles, while zero/low-emission zones received overall high encouragement. Furthermore, green public procurements were generally considered positively among all interviewees to help create an early market. Stricter demands and prolonged tendering processes should be considered in these processes. In assessing individual policy measures towards the criteria of effort, effectiveness, and acceptability, areas for improvement were identified. For facilitation of low-carbon infrastructure, effectiveness was found to likely improve if financial contributions exceed current mandates, targeting early adopters in urban areas, and offering operational support. Other challenges in Oslo’s URFT were linked to the need for authorities to clearly communicate what fuel propulsions are prioritised. Also, authorities should sometimes disregard the principle of technology neutrality, particularly relevant when supporting low-carbon technologies in an early phase. Further, the lack of delegating responsibility of URFT to a specific authority were identified as a drawback. Various levels and overlapping powers within political institutions ultimately begged the question of what specific body feel responsible for URFT. As such, creating a city logistics plan for Oslo should be the primary step, delegated to a specific agency or ministry both locally and nationally. Future research should focus on approaches between cities and best practices as to managing URFT. The sector is still in its infancy for what concerns political attention, on the backdrop of higher demand, emissions of GHG’s, other harmful pollutants, and negative side-effects such as noise

Electric Waterborne Public Transportation in Venice: a Case Study

The paper reports the results of a study for moving the present diesel-based watercraft propulsion technology used for public transportation in Venice city and lagoon to a more efficient and smart electric propulsion technology, in view of its adopted in a near future. Energy generation and storage systems, electrical machines and drives, as well as economic, environmental and social issues are presented and discussed. Some alternative solutions based on hybrid diesel engine and electric and full electric powertrains are compared in terms of weights, costs and payback times. Previews researches on ship propulsion and electric energy storage developed by the University of Padua and preliminary experiences on electric boats carried out in Venice lagoon by the municipal transportation company ACTV and other stakeholders are the starting point for this study. Results can be transferred to other waterborne mobility systems

NASA Innovative Advanced Concepts (NIAC): Heliopause Electrostatic Rapid Transit System (HERTS), Final Report

This report represents a summary of the study conducted under NASA Innovative Concept study contract number 14-NIAC14B-0075. The report provides a summary of the results of all contracted tasks and provides a suggested roadmap for continued development. The effort was collaborated with the Finnish Metrological Institute on an unfunded basis and the results of that coordination are reported herein. The Heliopause Electrostatic Rapid Transit System (HERTS) provides a flexible and enabling technology that can accelerate a spacecraft to velocities that allow travel times on the order of a decade for reaching the Heliopause; a feat that took the Voyager spacecraft(s) over 30 years to perform. The propulsion system concept being described is faster than any current propulsion system underdevelopment by NASA. The report describes the mission, the propulsion concept, and solar system trajectories. It also provides a comparison to the current state of the art in advanced propulsion concepts

Hybrid propulsion system with a gyro component for economic and dynamic operation

The design of a hybrid drive with gyro components is described and its drive components for a medium class private car are discussed. The gyro component affects the short-period output of the drive by accelerating and slowing down and -- because of the mechanical transfer of kinetic energy between the gyro and the vehicle -- it affects also the energy balance in the case of intermittent operation. Energy can be taken in as desired either in the form of fuel or as fuel and current. A high energy recovery efficiency as well as the favorable operating range of the interval combustion engine makes it possible to reduce the fuel consumption per unit distance travelled to almost half that for a private car with a traditional engine

Mass study for modular approaches to a solar electric propulsion module

The propulsion module comprises six to eight 30-cm thruster and power processing units, a mercury propellant storage and distribution system, a solar array ranging in power from 18 to 25 kW, and the thermal and structure systems required to support the thrust and power subsystems. Launch and on-orbit configurations are presented for both modular approaches. The propulsion module satisfies the thermal design requirements of a multimission set including: Mercury, Saturn, and Jupiter orbiters, a 1-AU solar observatory, and comet and asteroid rendezvous. A detailed mass breakdown and a mass equation relating the total mass to the number of thrusters and solar array power requirement is given for both approaches

Proposal and preliminary design for a high speed civil transport aircraft. Swift: A high speed civil transport for the year 2000

To meet the needs of the growing passenger traffic market in light of an aging subsonic fleet, a new breed of aircraft must be developed. The Swift is an aircraft that will economically meet these needs by the year 2000. Swift is a 246 passenger, Mach 2.5, luxury airliner. It has been designed to provide the benefit of comfortable, high speed transportation in a safe manner with minimal environmental impact. This report will discuss the features of the Swift aircraft and establish a solid, foundation for this supersonic transport of tomorrow

2020 NASA Technology Taxonomy: 2015 Technology Areas to 2020 Taxonomy Areas Crosswalk

To help users of the 2020 Taxonomy navigate changes from the 2015 Technology Area Breakdown Structure (TABS), this companion document provides a crosswalk between the 2015 Technology Areas (TAs) and the updated 2020 Taxonomy areas (TXs)

Solar sail science mission applications and advancement : solar sailing: concepts, technology, missions

Solar sailing has long been envisaged as an enabling or disruptive technology. The promise of open-ended missions allows consideration of radically new trajectories and the delivery of spacecraft to previously unreachable or unsustainable observation outposts. A mission catalogue is presented of an extensive range of potential solar sail applications, allowing identification of the key features of missions which are enabled, or significantly enhance, through solar sail propulsion. Through these considerations a solar sail application-pull technology development roadmap is established, using each mission as a technology stepping-stone to the next. Having identified and developed a solar sail application-pull technology development roadmap, this is incorporated into a new vision for solar sailing. The development of new technologies, especially for space applications, is high-risk. The advancement difficulty of low technology readiness level research is typically underestimated due to a lack of recognition of the advancement degree of difficulty scale. Recognising the currently low technology readiness level of traditional solar sailing concepts, along with their high advancement degree of difficulty and a lack of near-term applications a new vision for solar sailing is presented which increases the technology readiness level and reduces the advancement degree of difficulty of solar sailing. Just as the basic principles of solar sailing are not new, they have also been long proven and utilised in spacecraft as a low-risk, high-return limited-capability propulsion system. It is therefore proposed that this significant heritage be used to enable rapid, near-term solar sail future advancement through coupling currently mature solar sail, and other, technologies with current solar sail technology developments. As such the near-term technology readiness level of traditional solar sailing is increased, while simultaneously reducing the advancement degree of difficulty along the solar sail application-pull technology development roadmap