Commercial
Viability of the Next Generation
High-Speed Civil
Transport (HSCT)
By
GEORGE SAOUNATSOS
COPYRIGHT
1996
You may find the Abstract
and some compound Graphs of the above titled Report.
Click
HERE
for the full text on 'Technology Readiness and Development Risks'.
1. Abstract
The report investigates the
technological feasibility and economic viability of the Next Generation
High-Speed Civil Transport (HSCT), as the most important aspects of its
commercial success.
Realistic specifications
for the new SST call for a 2.2 Mach, 270 passengers, 5,500nm range aircraft.
The total cost of R&D is estimated at $15-20 billion with an actual
development period of 7-10 years. Improvements in aerodynamic analysis
methods promise an enhanced L/D ratio of about 45% in subsonic and 25%
in supersonic cruise. The resized increment in weight reduction due to
the elimination of the droop nose is estimated at 4,500kg. Adequate
sonic-boom reduction does not appear feasible at present. A 5-15%
lower specific fuel consumption is projected through the use of a variable
cycle engine, capable of generating acceptable (FAR 36 - Stage 3) community
noise. The Mixed-Flow Turbofan has been indicated by Americans as
a more likely engine to be used over the equally advantageous Mid-Tandem
Fan supported by Rolls Royce. The use of the Lean-Premixed-Prevaporized
or the Rich-burn/Quick-quench combustion processes could reduce the NOx
Emission Index to 5, resulting in less than 1% annual ozone depletion.
Studies indicate that 50% of passengers would accept an average 25% surcharge
over subsonic fares, while a 30-40% surcharge seems to be more pragmatic
for an adequately profitable HSCT. The estimated market needs of about
550 units by 2020 justify a satisfactory return on investment (12%) for
only one manufacturer. The unit cost should be about 1.8 times that of
the Boeing 747-400 in order to generate satisfactory profit for both airlines
and manufacturers. The corresponding yield, for a 12% ROI, could
then range between 11-13 cents/RPM.
Technology transfer through
a well structured international consortium would minimize the development
time and cost, establishing common environmental and certification rules.
The most probable Entry-Into-Service can be placed at 2010-2015.
Japan will play a determining role by selecting certain technology concepts
to finance, coming from Europe or the United States.
2. Graphs on economic-related
issues
 |
Figure 1: The starting
point in the economic assessment is the technical characteristics of the
aircraft, which reflect the performance and its capabilities. Several
factors can then be determined, such as the potential network based on
the cruise Mach number and aircraft range, or the block fuel required as
derived by the specific fuel consumption (SFC). In parallel, the
number of seats available determines the potential scheduling, while the
utilization rate and stimulation enter the picture as a function of the
routing chosen. Furthermore, the constraints applied in the operation
of supersonic vehicles directly affect the scheduling of the HSCT and the
network that can be operated profitably. This network is also based
on the projected traffic of each route, which ensures that there is a sufficient
volume to support the operation of supersonic transports. Additional
key elements in the economic success of the future HSCT are the value of
the supersonic fare and the corresponding passenger share, which are directly
related to the Total Operating Cost (TOC) of the aircraft. At the
same time the production cost, as affected by the total number of aircraft
required, determines the unit acquisition price. It also plays a
fundamental role in the total operating cost of the HSCT, closing in this
way a decisive economic loop for its success. In other words, the
next generation HSCT must be economically competitive with the subsonic
fleet, in order to be able to earn a return on investment (ROI) at least
similar to the return that could be earned by operating subsonic airplanes
on the same route system. This concept is fundamental to the analysis
methods used in evaluating the economic worth of the future HSCT aircraft.
 |
Figure 2: An investigation
made by the Boeing company resulted in some preliminary elasticity demand
curves, which relate ticket price to market share as a function of time
saved. The initial data were collected from four surveys conducted
on a 50-50 mix of business and economy class travelers. The results
indicate that the percentage of passengers choosing supersonic service
decreases substantially as the price is increased. At the same time,
the percentage of travelers willing to go supersonic increases as time
savings become larger. From the above graph can be observed that
for a 40% time saving, a 10% ticket price increase would reduce the market
share by over 65%. When elasticity curves, however, are more accurately
established for all specific HSCT market segments, airlines would be able
to calculate possible yields from a mixture of subsonic and supersonic
flights. Varying the surcharge for supersonic service could be certainly
used to optimize the traffic volume and mix for highest profit potential.
[SOURCE:
Boeing]
 |
Figure 3: Focusing
in the relation between the development cost, the potential number of aircraft
required and the unit cost as a function of the design range, the compound
chart presented above gives a thorough understanding of the resulted interdependency.
For large design ranges the development cost increases, dragging up the
unit price and lowering the amount of units required. Consequently,
passenger share decreases as a result of higher ticket prices, although
a larger range capability could accommodate the needs of a larger public,
i.e. a higher market share. For a 5,000nm-range HSCT can be observed
that about 700 units are needed at an average price of about US$ 260 million.
At this number of required HSCTs, the aircraft cost could be 1.4 times
that of the VLA, or almost 2 times that of the Boeing 747-400. [SOURCE:
JADC - Japan Aircraft Development Corporation]
 |
Figure 4: In another
sensitivity study, Boeing related fleet size variability to the required
yield to achieve a 12% return on investment. For this study, was
assumed that if a modest increase of 10% was made in the first and business
class passengers' fare, and if the their corresponding class sections of
the airplane were expanded so that the economy-class demand was not entirely
accommodated, then the revenue level would be "enriched" by the enlarged
percentage of the higher priced fare classes. In parallel, the potential
surcharge on economy passengers was varied as above. It can be noticed
that the per passenger yield level, required to meet the ROI target, increases
as market share drops. That is because there are fewer passengers
on any given route and the physical airplane remains the same. On
the other hand, with about an 18% economy ticket price increase and 22%
economy market share, the yield required for a 12% ROI equals the yield
available. The next generation HSCT, however, becomes economically
viable with a 49% market share and a worldwide sales of 650 to 700 units.
This amount is perceived as the bottom line of the economic evaluation
of the Boeing company, suggesting that while it reflects an adequate demand
for a single manufacturer, it is not adequate for two or more. The
tactic of yield "enrichment", however, brings with it operational problems
from the airline's perspective by excluding economy class passengers.
For example, an airline operating an HSCT which accommodates less than
half the total demand, would have to provide another subsonic aircraft
type on the same route to carry the remaining demand, probably consisting
of mostly low fare classes. The fleet efficiency may therefore be
reduced by the requirement to provide two airplane types to serve a single
market. [SOURCE: Boeing]
A similar passenger-class
oriented approach was followed by Deutsche Aerospace-Airbus. DASA
examined the operation of a fleet of HSCTs in consideration of a standard
class mix used in subsonic transports, as well as a supersonic class-mix
where discount fares were totally banned (figure 5).
 |
Figure 5: It can
be observed that surcharges on subsonic ticket prices determine the market
share and thus the number of aircraft put into service. When the
fare premiums are set to cover just the extra operational cost, it is indicated
that about 800 HSCTs are required with a 30% surcharge applied. Whereas
the tendency of the manufacturers would be clearly to maximize the number
of aircraft produced and sold, the airlines would more likely follow a
strategy to maximize the extra profit from HSCT operation. For extra
yield therefore, in the order of 13%, higher surcharges (.40%) at standard
subsonic class mix could reduce the total fleet size to about 400 aircraft.
Alternatively, yields could be improved by banning discount fares through
the use of the more attractive supersonic class mix, leading to lower surcharges
(.18%) in the remaining ticket types. This effect would again result
in a fleet of about 800 HSCTs, and a price ratio of about 1.8 to the Boeing
747-400.
[SOURCE: DASA]
