Bristol Spaceplanes

Last updated

Bristol Spaceplanes Ltd.
Type Private
Industry Aerospace
Founded1991
Key people
David Ashford (Managing Director)
Products Space tourism, Spaceplanes
Website http://www.bristolspaceplanes.com/

Bristol Spaceplanes (BSP) is a British aerospace company based in Bristol, England, who has designed a number of spaceplanes with sub-orbital and orbital capabilities. The company's stated goal is "to realise low-cost access to space", [1] primarily through reusable launch vehicles, claiming the cost of human space travel has the potential to be reduced by a factor of 1,000. [2]

Contents

History

The company was founded in 1991 by David Ashford and has received three feasibility grants in 1993, 2003 and 2011 for the Ascender and Spacecab projects. [1] A scaled down radio-controlled version of the Ascender spaceplane was successfully flown in 1998.

In the early 2000s, Bristol Spaceplanes Limited was an unsuccessful entrant in the Ansari X-Prize competition to be the first private crewed spaceflight vehicle to launch and relaunch in a week, losing out to Mojave Aerospace Ventures' Tier One combo of SpaceShipOne and WhiteKnightOne. [3]

In September 2014 the firm launched a crowdfunding campaign to aid in the development of Ascender, aiming to raise £150,000. [4] [5] [ needs update ]

In late 2014, the company was conducting bench testing of rocket engine designs for Ascender and is seeking funding to build a working model via crowdfunding. [6]

Throughout the lifetime of the company David Ashford has released a number of published books and papers based around the aerospace industry and the exploration of space. [7] [8] [9]

Conceptual vehicles and spacecraft

Ascender

Ascender is a proposed small two-seater suborbital horizontal-takeoff, horizontal-landing (HTHL), jet- and rocket-powered spaceplane concept which is designed to be able to achieve altitudes of up to 100 kilometres (62 mi) via a steep sub-orbital trajectory. [10]

This would allow it to be used for space tourism activity as well as microgravity research during the two minutes of weightlessness. The vehicle would take off[ when? ] from a typical runway using its two turbofan jet engines and climb to cruising altitudes. It would then switch to its hydrogen peroxide rocket engine and climb past 80 kilometres (50 mi) and then would reenter the atmosphere and glide back to the runway it took off from, using its jet engines to maneuver.

The majority of attention and energy of the company has been focused on the Ascender launcher due to its short-term feasibility compared to the other projects. It has been designed to not require any new materials or unproven components. [10]

Spacecab

The Spacecab spaceplane design concept consists of a large crewed "carrier" aircraft with a smaller "orbiter" attached on top, both of which are derived from Ascender. The carrier would take off from an airstrip and use its turbofan engines to accelerate to mach 2 at which point it would switch over to its LOX/Kerosene rocket engines to accelerate to mach 4. The orbiter craft would then detach and accelerate to orbital speeds and altitudes using its LOX/LH2 rocket. It would be capable of delivering up to 750 kg to low Earth orbit, and also transporting supplies and crew to the International Space Station, an increasingly important capability following the retirement of the Space Shuttle. Spacecab can be thought of as the intermediate next step in development between Ascender and Spacebus, and like Ascender it does not require any new technology or materials and has been the subject of a 1994 feasibility study confirming this claim. [11]

Spacebus

The Spacebus spaceplane concept is the largest, most ambitious, costly, and difficult project proposed by the company. It has a similar, but scaled-up design to Spacecab with a "carrier" craft accelerating up to mach 4 with Ramjet engines and then up to mach 6 with rocket engines. The smaller "orbiter" would then detach and accelerate into orbit with LOX/LH2 rocket engines with a payload of up to 5000 kg or 50 passengers. Despite requiring a new Ramjet design and significant developments with the heatshield, rocket engines, hydrogen fuel system, and transparencies, Spacebus is still claimed to be more feasible than other ongoing spaceplane projects. [12]

See also

Related Research Articles

British Aerospace HOTOL UK Spaceplane design of 1980s

HOTOL, for Horizontal Take-Off and Landing, was a 1980s British design for a single-stage-to-orbit (SSTO) spaceplane that was to be powered by an airbreathing jet engine. Development was being conducted by a consortium led by Rolls-Royce and British Aerospace (BAe).

Aerospike engine Type of rocket engine that maintains its aerodynamic efficiency across a wide range of altitudes

The aerospike engine is a type of rocket engine that maintains its aerodynamic efficiency across a wide range of altitudes. It belongs to the class of altitude compensating nozzle engines. A vehicle with an aerospike engine uses 25–30% less fuel at low altitudes, where most missions have the greatest need for thrust. Aerospike engines have been studied for several years and are the baseline engines for many single-stage-to-orbit (SSTO) designs and were also a strong contender for the Space Shuttle main engine. However, no such engine is in commercial production, although some large-scale aerospikes are in testing phases.

Scramjet Jet engine where combustion takes place in supersonic airflow

A scramjet is a variant of a ramjet airbreathing jet engine in which combustion takes place in supersonic airflow. As in ramjets, a scramjet relies on high vehicle speed to compress the incoming air forcefully before combustion, but whereas a ramjet decelerates the air to subsonic velocities before combustion using shock cones, a scramjet has no shock cone and slows the airflow using shockwaves produced by its ignition source in place of a shock cone. This allows the scramjet to operate efficiently at extremely high speeds.

Spaceplane Spacecraft capable of aerodynamic flight in atmosphere

A spaceplane is a vehicle that can fly and glide like an aircraft in Earth's atmosphere and maneuver like a spacecraft in outer space. To do so, spaceplanes must incorporate features of both aircraft and spacecraft. Orbital spaceplanes tend to be more similar to conventional spacecraft, while sub-orbital spaceplanes tend to be more similar to fixed-wing aircraft. All spaceplanes to date have been rocket-powered but then landed as unpowered gliders.

Skylon (spacecraft) Single-stage-to-orbit spaceplane

Skylon is a series of concept designs for a reusable single-stage-to-orbit spaceplane by the British company Reaction Engines Limited (Reaction), using SABRE, a combined-cycle, air-breathing rocket propulsion system. The vehicle design is for a hydrogen-fuelled aircraft that would take off from a purpose-built runway, and accelerate to Mach 5.4 at 26 kilometres (85,000 ft) altitude using the atmosphere's oxygen before switching the engines to use the internal liquid oxygen (LOX) supply to take it into orbit. It could carry 17 tonnes (37,000 lb) of cargo to an equatorial low Earth orbit (LEO); up to 11 tonnes (24,000 lb) to the International Space Station, almost 45% more than the capacity of the European Space Agency's Automated Transfer Vehicle; or 7.3 tonnes (16,000 lb) to Geosynchronous Transfer Orbit (GTO), over 24% more than SpaceX Falcon 9 launch vehicle in reusable mode. The relatively light vehicle would then re-enter the atmosphere and land on a runway, being protected from the conditions of re-entry by a ceramic composite skin. When on the ground, it would undergo inspection and necessary maintenance, with a turnaround time of approximately two days, and be able to complete at least 200 orbital flights per vehicle.

NASA X-43 Unmanned US experimental hypersonic aircraft, 2001-2004

The NASA X-43 was an experimental unmanned hypersonic aircraft with multiple planned scale variations meant to test various aspects of hypersonic flight. It was part of the X-plane series and specifically of NASA's Hyper-X program. It set several airspeed records for jet aircraft. The X-43 is the fastest jet-powered aircraft on record at approximately Mach 9.6.

Lockheed Martin X-33 Uncrewed re-usable spaceplane technology demonstrator for the VentureStar

The Lockheed Martin X-33 was an uncrewed, sub-scale technology demonstrator suborbital spaceplane developed in the 1990s. The X-33 was a technology demonstrator for the VentureStar orbital spaceplane, which was planned to be a next-generation, commercially operated reusable launch vehicle. The X-33 would flight-test a range of technologies that NASA believed it needed for single-stage-to-orbit reusable launch vehicles, such as metallic thermal protection systems, composite cryogenic fuel tanks for liquid hydrogen, the aerospike engine, autonomous (uncrewed) flight control, rapid flight turn-around times through streamlined operations, and its lifting body aerodynamics.

SABRE (rocket engine) Synergetic Air Breathing Rocket Engine - a hybrid ramjet and rocket engine

SABRE is a concept under development by Reaction Engines Limited for a hypersonic precooled hybrid air-breathing rocket engine. The engine is being designed to achieve single-stage-to-orbit capability, propelling the proposed Skylon spaceplane to low Earth orbit. SABRE is an evolution of Alan Bond's series of LACE-like designs that started in the early/mid-1980s for the HOTOL project.

XCOR Aerospace American private rocket engine and spaceflight development company

XCOR Aerospace was an American private spaceflight and rocket engine development company based at the Mojave Air and Space Port in Mojave, California, Midland International Air and Spaceport in Midland, Texas and the Amsterdam area, the Netherlands. XCOR was formed in 1999 by former members of the Rotary Rocket rocket engine development team, and ceased operations in 2017.

Reaction Engines British aerospace company based in Oxfordshire, England

Reaction Engines Limited is a British aerospace manufacturer based in Oxfordshire, England.

The Tupolev Tu-2000 was a planned hypersonic flight experimental aircraft designed by the Tupolev design bureau. It was intended to test technologies for a single-stage-to-orbit aerospaceplane and also the Tupolev Tu-360 intercontinental bomber.

Project 921-3 is a crewed spacecraft sub-system of Project 921. The term 921-3 is often used for the Chinese spaceplane program.

The Keldysh bomber was a Soviet design for a rocket-powered sub-orbital bomber spaceplane, which drew heavily upon work carried out by Eugen Sänger and Irene Bredt for the German Silbervogel project.

XCOR Lynx

The XCOR Lynx was a proposed suborbital horizontal-takeoff, horizontal-landing (HTHL), rocket-powered spaceplane that was under development by the California-based company XCOR Aerospace to compete in the emerging suborbital spaceflight market. The Lynx was intended to carry one pilot, a ticketed passenger, and/or a payload above 100 km altitude. The concept was under development since 2003, when a two-person suborbital spaceplane was announced under the name Xerus.

Air-launch-to-orbit Method of launching rockets at altitude from a conventional horizontal-takeoff aircraft

Air launch to orbit is the method of launching rockets at altitude from a conventional horizontal-takeoff aircraft, to carry satellites to low Earth orbit. It is a follow-on development of air launches of experimental aircraft that began in the late 1940s. This method, when employed for orbital payload insertion, presents significant advantages over conventional vertical rocket launches, particularly because of the reduced mass, thrust and cost of the rocket.

SpaceLiner German concept space hypersonic airliner

SpaceLiner is a concept for a suborbital, hypersonic, winged passenger supersonic transport, conceived at the German Aerospace Center in 2005. In its second role the SpaceLiner is intended as a reusable launch vehicle (RLV) capable of delivering heavy payloads into orbit.

The DARPA XS-1 was an experimental spaceplane/booster with the planned capability to deliver small satellites into orbit for the U.S. Military. It was reported to be designed to be reusable as frequently as once a day, with a stated goal of doing so for 10 days straight. The XS-1 was intended to directly replace the first stage of a multistage rocket by taking off vertically and flying to hypersonic speed and high suborbital altitude, enabling one or more expendable upper stages to separate and deploy a payload into low Earth orbit. The XS-1 would then return to Earth, where it could ostensibly be serviced fast enough to repeat the process at least once every 24 hours.

Space Engine Systems Inc. (SES) is a Canadian aerospace company and is located in Edmonton, Alberta, Canada. The main focus of the company is the development of a light multi-fuel propulsion system to power a reusable single-stage-to-orbit (SSTO) and hypersonic cruise vehicle. Pumps, compressors, gear boxes, and other related technologies being developed are integrated into SES's major R&D projects. SES is collaborating with the University of Calgary to study and develop technologies in key technical areas of nanotechnology and high-speed aerodynamics.

Saenger (spacecraft)

Saenger or Sänger was a West German concept design for a two-stage-to-orbit spaceplane. It is named after Eugen Sänger, who had been a key figure in the development of the concept for aerospace company Junkers.

WIRES is a Japanese project developing a winged single-stage reusable suborbital rocket as a test bed for a reusable orbital launch system or a crewed suborbital spaceplane. The full-size prototype, called WIRES-X, is expected to be launched in 2020.

References

  1. 1 2 "Bristol Spaceplanes Company Information". Bristol Spaceplanes. 2014. Archived from the original on 4 July 2014. Retrieved 11 September 2014.
  2. "Bristol Spaceplanes joins tourism race". The Financial Times. 2014. Retrieved 11 September 2014.
  3. "Ansari X-Prize Teams". X-Prize Foundation. 2014.
  4. "The Market For Bristol Spaceplanes". Bristol Spaceplanes. 2014. Retrieved 11 September 2014.
  5. Bristol firm enters commercial space race Daily Telegraph 23 February 2014
  6. "Bristol Spaceplanes Crowdfunder" . Retrieved 19 December 2014.
  7. "Space Exploration- All that Matters". Bristol Spaceplanes. 2014. Retrieved 11 September 2014.
  8. "Spaceflight Revolution". Bristol Spaceplanes. 2014. Retrieved 11 September 2014.
  9. "Your Spaceflight Manual/". Bristol Spaceplanes. 2014. Retrieved 11 September 2014.
  10. 1 2 "Ascender Project Specifications/". Bristol Spaceplanes. 2014. Retrieved 11 September 2014.
  11. "Spacecab Project Specifications/". Bristol Spaceplanes. 2014. Retrieved 11 September 2014.
  12. "Spacebus Project Specifications/". Bristol Spaceplanes. 2014. Retrieved 11 September 2014.