Hypersonic Transport Vehicles

Roadmap & System Overview

Hypersonic transport vehicles are a type of aircraft from the wider group of hypersonic systems. Hypersonic systems are all vehicles that operate in the flight regime where aerodynamic heating becomes significant, typically thought of as flight faster than Mach 5. Such systems include most atmospheric entry vehicles, some orbital launch vehicles, and several types of ballistic or maneuvering missiles. Hypersonic transport vehicles aim to move personnel and cargo from place to place much faster than traditional transonic or even supersonic aircraft. With a commercial application, this would be accomplished with the aim of generating profit for the company providing the transport service.

This page presents a technology roadmap for hypersonic transport vehicles. Hypersonic systems rely upon a myriad of sub-technologies that have allowed us to perfect flight at lower Mach numbers. Several of these existing technologies will be discussed here, in addition to a critical review of the technology advances still required to enable commercial hypersonic transport vehicles.

Boeing hypersonic airliner concept, from Wired, "Boeing’s Proposed Hypersonic Plane Is Really, Really Fast" by Eric Adams, published June 28, 2018. https://www.wired.com/story/boeing-hypersonic-mach-5-jet-concept/

Design Structure Matrix Allocation

A hierarchical breakdown of a subset of the technologies required to enable the development of hypersonic transport vehicles is shown below. Note that the level 1 hypersonic transport vehicle technology is decomposed into four level two sub-technologies: vehicle structures, combined-cycle engines, high-temperature materials, and integrated modeling environments.

It is noted that several interactions exist between the various sub-technologies shown below. Such interactions are indicated in the design structure matrix (DSM), shown below. Interactions shown in grey represent either physical or component-type linkages (i.e. high-speed wings are part of hypersonic transport vehicles), whereas interactions in yellow represent information flows (i.e. aero-thermal analysis models are required for the development of high-speed wings).

Roadmap Model Using Object-Process Methodology (OPM)

An OPM diagram showing a sample of the processes required for the creation and operation of commercial hypersonic transport vehicles is shown below. Note that the technology of interest (hypersonic transport vehicle) is shown near the center of the figures. The hypersonic transport vehicle serves to transport passengers from one location to another (also indicated near the center of the diagram). FOMs are shown towards the bottom right, with connections to relevant processes. It is noted that the sub-technologies shown in the diagram (high-temperature materials and structures, variable fidelity modeling, and combined-cycle engines) are discussed in detail by Bowcutt in [5].

Figures of Merit

The figures of merit (FOMs) relevant to commercial hypersonic transports include the distance covered per time (speed, v), aircraft range R, operating cost per flight C_O, the aircraft profit per flight p, the number of flights per aircraft, and the trans-Atlantic flight time. The profit p generated by the airline may be the single most important figure of merit, as it is the ultimate driver for the existence of commercial hypersonic vehicles (without profit, airlines will not offer such a service). These FOMs are described in the table below.

Figure of Merit (FOM)	Unit	Description
Aircraft Speed	[m/s]	Maximum velocity of the aircraft during the flight. Correlates to cruise velocity for hypersonic commercial transport vehicles.
Aircraft Range	[m]	Maximum distance traveled per flight at maximum payload capacity.
Operating Cost	[$]	Cost per flight to operate the aircraft. Function of the personnel (pilot and crew) cost, fuel cost and post-flight refurbishment required prior to future flights.
Profit per Flight	[$]	Function of the number of passengers, price per ticket, operating cost and overall programmatic cost.
Flights per Aircraft	[n]	Number of flights will be limited by structural fatigue due to system cycles.
Trans-Atlantic Flight Time	[hrs]	A function of aircraft velocity that captures the transitions between takeoff, cruise, and landing phases of flight. Because of the length of the transient phases (takeoff and landing), this FOM more directly correlates to the benefit to the consumer than the aircraft velocity FOM.

<math>v=$$\frac{d}{t}$$</math>

The FOMs above are described mathematically, including expected nominal values in the table below.

Figure of Merit (FOM)	Unit	Mathematical Equation	Nominal Values
Aircraft Speed	[m/s]	<math>v=\frac{d}{t}</math>	3,350 [m/s] (Mach 5 @ 30,000 ft cruise alt.)
Aircraft Range	[m]
Operating Cost	[$]
Profit per Flight	[$]
Flights per Aircraft	[n]
Trans-Atlantic Flight Time	[hrs]