OTRAG

Last updated
OTRAG
IndustryAlternative propulsion system for rockets
Founded1974 (1974) in Neu-Isenburg, West Germany
FounderLutz Kayser
Defunct1987
FateNationalized by Libya
Headquarters
Stuttgart
,
West Germany
Area served
West Germany, Zaire, Libya
Key people
Lutz Kayser
Kurt H. Debus
Frank Wukasch
Wolfgang Pilz
Wernher von Braun

OTRAG (German: Orbital Transport-und Raketen-Aktiengesellschaft, [1] [2] or Orbital Transport and Rockets, Inc.), was a West German company based in Stuttgart, which in the late 1970s and early 1980s planned to develop an alternative propulsion system for rockets. OTRAG was the first commercial developer and producer of space launch vehicles. The OTRAG Rocket claimed to present an inexpensive alternative to existing launch systems through mass-production of Common Rocket Propulsion Units (CRPU).

Contents

History

OTRAG was founded on October 17, 1974 [3] by German aerospace engineer Lutz Kayser. OTRAG's goal was to develop, produce, and operate a low-cost satellite launch vehicle. It was the first private company to attempt to launch a private spacecraft. [4] The OTRAG rocket was intended to be an inexpensive alternative to the European rocket Ariane and the NASA Space Shuttle. [5] Kayser and a private consortium of six hundred European investors financed the development and production of the OTRAG satellite launch vehicle. Dr. Kurt H. Debus served as Chairman of the Board of OTRAG (1974–1980) after his retirement as director of NASA's Kennedy Space Center, [6] [7] and Dr. Wernher von Braun served as scientific adviser to Kayser.

In the face of doubts by Debus and von Braun, Kayser chose in 1975 to set up testing and launch facilities in Shaba, Zaire (now Katanga Province, Democratic Republic of the Congo). Debus and von Braun were concerned about the possibility of Zairian acquisition of missile technology from the facilities. Kayser decided to proceed despite their opposition.

Otrag's first test was on May 17, 1977, with the second successful launch on May 20, 1978. The third test failed on June 5, with Zairian President Mobutu Sese Seko watching the launch. [8]

Political pressure to halt the company's operations mounted quickly. France and the Soviet Union were historically opposed to German long-distance rocket development and pressured the Zairian government into closing down the development facility in 1979. Immediately afterwards, Presidents Giscard d'Estaing of France and Leonid Brezhnev of the Soviet Union convinced the West German government to cancel the OTRAG project and close down its German operations. In 1980, OTRAG moved its production and testing facilities to a desert site in Libya. A series of successful tests was conducted at this site beginning in 1981. [9]

OTRAG shut down in 1987. [8] As the company left Libya, Muammar Gaddafi confiscated all equipment and installations, hoping to later use the technology, and German investors lost their money. [10]

Rocket design

OTRAG OTRAG rocket concept shape-02.jpg
OTRAG
OTRAG CRPU OTRAG CRPU shape.jpg
OTRAG CRPU

OTRAG was a design quite different from conventional multistage rockets. The OTRAG design used parallel stages assembled from parallel tank tubes with flat bulkheads. The rockets were designed to carry loads up to two tons, the then usual weight of a communications satellite, into a geostationary orbit. It was planned to later increase the capacity to ten tons or more using multiple identical modules. [11]

The rocket was to consist of individual pipes, each 27 cm in diameter and six meters long. Four of these pipes would be installed one above the other resulting in a 24 meter long fuel and oxidizer tank with a rocket engine at the lower end making up a CRPU. The fuel was intended to be kerosene with a 50/50 mixture of nitric acid and dinitrogen tetroxide as an oxidiser. Ignition was provided by a small quantity of furfuryl alcohol injected before the fuel, which ignites hypergolically (immediately and energetically) upon contact with the nitric acid. To simplify the design, pumps were not used to move the fuel to the engines, instead the fuel tanks were only 66% filled, with compressed air in the remaining space to press propellants into the ablatively cooled combustion chamber. Thrust control is by partially closing the electromechanical propellant valves. Pitch and yaw control can thus be achieved by differential throttling. In principle this is extremely reliable and cheap in mass production.

The modular design was intended to result in a large cost reduction due to economies of scale. The CRPU-based satellite launching rocket was estimated to cost approximately one tenth of conventional designs. Automated production processes for all components would reduce labor cost from 80% to 20% and remove the justification for reusability of spent stages.

One large 4 stage configuration OTRAG 10K [11] was supposed to launch a payload of 10,000 kg to a 185 km Orbit. The planned liftoff thrust was around 26 MN with a total mass of 2,300 tonnes:

Controversies and future outlook

Only a few political controversies are known concerning OTRAG, which involve the concerns of neighbors in Zaire and Libya about the dual use potential of rockets. A full orbital launch vehicle was never assembled. Modules were flight tested in Zaire and Libya. 6,000 static rocket engine tests and 16 single-stage qualification tests were made to prove the concept as feasible [ citation needed ].

Hans Dietrich Genscher, the then-minister of German foreign affairs, is said to have finally stopped the project under pressure from France and the Soviet Union,[ citation needed ] and West Germany joined the co-financed "European rocket" Ariane project, which made the OTRAG project unnecessary and eliminated political entanglements of a still divided Germany in the early 1980s.

Around 2009, Lutz Kayser had been advising Interorbital Systems, resulting in a similar modular rocket design for their Neptune series. [12]

John Carmack, founder and lead engineer of Armadillo Aerospace has stated in his monthly reports and in forum posts that he expected his path to an orbital vehicle to include modular rockets similar to OTRAG technology. Kayser, being the founding engineer of OTRAG, visited Armadillo in May, 2006 and loaned Carmack some of their original research hardware.

"I have been corresponding with Lutz [Kayser] for a few months now, and I have learned quite a few things. I seriously considered an OTRAG style massive-cluster-of-cheap-modules orbital design back when we had 98% peroxide (assumed to be a biprop with kerosene), and I have always considered it one of the viable routes to significant reduction in orbital launch costs. After really going over the trades and details with Lutz, I am quite convinced that this is the lowest development cost route to significant orbital capability. Eventually, reusable stages will take over, but I actually think that we can make it all the way to orbit on our current budget by following this path. The individual modules are less complicated than our current vehicles, and I am becoming more and more fond of high production methods over hand crafter prototypes." -- Carmack June 2006 Armadillo Aerospace Update [13]

See also

Related Research Articles

<span class="mw-page-title-main">Expendable launch system</span> Launch system that uses a single use launch vehicle

An expendable launch system is a launch vehicle that can be launched only once, after which its components are either destroyed during reentry or discarded in space. ELVs typically consist of several rocket stages that are discarded sequentially as their fuel is exhausted and the vehicle gains altitude and speed. As of 2022, most satellites and human spacecraft are currently launched on ELVs. ELVs are simpler in design than reusable launch systems and therefore may have a lower production cost. Furthermore, an ELV can use its entire fuel supply to accelerate its payload, offering greater payloads. ELVs are proven technology in widespread use for many decades.

<span class="mw-page-title-main">Proton (rocket family)</span> Russian (formerly Soviet) rocket family

Proton is an expendable launch system used for both commercial and Russian government space launches. The first Proton rocket was launched in 1965. Modern versions of the launch system are still in use as of 2023, making it one of the most successful heavy boosters in the history of spaceflight. The components of all Protons are manufactured in the Khrunichev State Research and Production Space Center factory in Moscow and Chemical Automatics Design Bureau in Voronezh, then transported to the Baikonur Cosmodrome, where they are assembled at Site 91 to form the launch vehicle. Following payload integration, the rocket is then brought to the launch pad horizontally by rail, and raised into vertical position for launch.

<span class="mw-page-title-main">Armadillo Aerospace</span> American aerospace startup company

Armadillo Aerospace was an aerospace startup company based in Mesquite, Texas. Its initial goal was to build a crewed suborbital spacecraft capable of space tourism, and it had also stated long-term ambitions of orbital spaceflight. The company was founded by John Carmack, co-founder and former chief technical officer of id Software.

Big Dumb Booster (BDB) is a general class of launch vehicle based on the premise that it is cheaper to operate large rockets of simple design than it is to operate smaller, more complex ones regardless of the lower payload efficiency. As referred to by the Office of Technology Assessment:

The term Big Dumb Booster has been applied to a wide variety of concepts for low-cost launch vehicles, especially those that would use "low technology" approaches to engines and propellant tanks in the booster stage. As used here, it refers to the criterion of designing launch systems for minimum cost by using simplified subsystems where appropriate.

<span class="mw-page-title-main">Vega (rocket)</span> European Space Agency launch system

Vega is an expendable launch system in use by Arianespace jointly developed by the Italian Space Agency (ASI) and the European Space Agency (ESA). Development began in 1998 and the first launch took place from the Guiana Space Centre on 13 February 2012.

<span class="mw-page-title-main">Spaceplane</span> 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 for takeoff and climb, but have then landed as unpowered gliders.

The Saturn I was a rocket designed as the United States' first medium lift launch vehicle for up to 20,000-pound (9,100 kg) low Earth orbit payloads. The rocket's first stage was built as a cluster of propellant tanks engineered from older rocket tank designs, leading critics to jokingly refer to it as "Cluster's Last Stand". Its development was taken over from the Advanced Research Projects Agency in 1958 by the newly formed civilian NASA. Its design proved sound and flexible. It was successful in initiating the development of liquid hydrogen-fueled rocket propulsion, launching the Pegasus satellites, and flight verification of the Apollo command and service module launch phase aerodynamics. Ten Saturn I rockets were flown before it was replaced by the heavy lift derivative Saturn IB, which used a larger, higher total impulse second stage and an improved guidance and control system. It also led the way to development of the super-heavy lift Saturn V which carried the first men to landings on the Moon in the Apollo program.

The Vanguard rocket was intended to be the first launch vehicle the United States would use to place a satellite into orbit. Instead, the Sputnik crisis caused by the surprise launch of Sputnik 1 led the U.S., after the failure of Vanguard TV-3, to quickly orbit the Explorer 1 satellite using a Juno I rocket, making Vanguard 1 the second successful U.S. orbital launch.

<span class="mw-page-title-main">Angara (rocket family)</span> Russian family of space launch vehicles

The Angara rocket family is a family of launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center. The launch vehicles are to put between 3,800 kg (8,400 lb) and 24,500 kg (54,000 lb) into low Earth orbit and are intended, along with Soyuz-2 variants, to replace several existing launch vehicles.

<span class="mw-page-title-main">Pressure-fed engine</span> Rocket engine operation method

The pressure-fed engine is a class of rocket engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and oxidizer to the combustion chamber. To maintain adequate flow, the tank pressures must exceed the combustion chamber pressure.

<span class="mw-page-title-main">Interorbital Systems</span>

Interorbital Systems (IOS) is an American company based in Mojave, California that specializes in the manufacturing of rockets and satellites. It was established in 1996 by Roderick and Randa Milliron. As of October 2023, the company is in development stage for three orbital launch vehicles: NEPTUNE, TRITON, and TRITON HEAVY.

<span class="mw-page-title-main">OTRAG (rocket)</span>

The OTRAG rocket was a modular satellite-delivery rocket developed by the OTRAG company in the 1970s and 80s. The OTRAG rocket was to become a rocket built up from several mass-produced units, intended to carry satellites with a weight of 1-10 tons or more into orbit. Mass production meant that the vehicle was projected to have been 10x cheaper than conventional vehicles of similar capability.

<span class="mw-page-title-main">ARCAspace</span> Aerospace company headquartered in Romania

Romanian Cosmonautics and Aeronautics Association, also known as ARCAspace, is an aerospace company based in Râmnicu Vâlcea, Romania. It builds rockets, high-altitude balloons, and unmanned aerial vehicles. It was founded in 1999 as a non-governmental organization in Romania by the Romanian engineer and entrepreneur Dumitru Popescu and other rocket and aeronautics enthusiasts. Since then, ARCA has launched two stratospheric rockets and four large-scale stratospheric balloons including a cluster balloon. It was awarded two governmental contracts with the Romanian government and one contract with the European Space Agency. ARCASpace is currently developing a three-stage, semi-reusable steam-powered rocket called EcoRocket and in 2022 has shifted its business model to Asteroid mining.

<span class="mw-page-title-main">Fuji (spacecraft)</span> Japanese proposed manned spacecraft

Fuji (ふじ) was a crewed spacecraft of the space capsule kind, proposed by Japan's National Space Development Agency (NASDA) Advanced mission Research center in December 2001. The Fuji design was ultimately not adopted.

<span class="mw-page-title-main">Athena (rocket family)</span> Lockheed Martin expendable launch system

Athena was a 1990s Lockheed Martin expendable launch system which underwent several name changes in its lifetime.

The VLS-1 was the Brazilian Space Agency's main satellite launch vehicle. The launch vehicle would have been capable of launching satellites into orbit. The launch site was located at the Alcântara Launch Center due to its proximity to the equator.

<span class="mw-page-title-main">Space tug</span> Spacecraft used to transfer cargo from one orbit to another

A space tug is a type of spacecraft used to transfer spaceborne cargo from one orbit to another orbit with different energy characteristics. The term can include expendable upper stages or spacecraft that are not necessarily a part of their launch vehicle. However, it can also refer to a spacecraft that transports payload already in space to another location in outer space, such as in the Space Transportation System concept. An example would be moving a spacecraft from a low Earth orbit (LEO) to a higher-energy orbit like a geostationary transfer orbit, a lunar transfer, or an escape trajectory.

<span class="mw-page-title-main">VLM (rocket)</span> Proposed Brazilian satellite launcher

The VLM is a proposed three-stage satellite launcher being developed by the Brazilian General Command for Aerospace Technology in collaboration with Germany. The project originated in 2008 as a simplified version of the VLS-1 rocket, using only the core stages. The first launch is currently planned for no earlier than 2027.

Exos Aerospace Systems & Technologies is an aerospace manufacturer and developer of reusable launch systems intended to support uncrewed orbital spaceflight launches, and is based in Caddo Mills, Texas.

bluShift Aerospace American aerospace firm

BluShift Aerospace is an employee-owned American aerospace firm based in Brunswick, Maine. Targeting the growing smallsat and cubesat launch markets, bluShift is developing suborbital sounding rockets and small-lift orbital rockets which will be launched from a proposed new spaceport in Maine. The company has received primary funding from NASAs SBIR grant program, the National Science Foundations I-Corps grant program, the Maine Technology Institute, and the Maine Space Grant Consortium. The company has active operations at the former Brunswick Naval Air Station and Loring Air Force Base.

References

  1. Miller, Judith (September 12, 1981). "U.S. Uneasy Over Military Potential Of Commercially Produced Rockets". The New York Times . Retrieved December 20, 2022.
  2. Schneiker, Conrad (February 1978). "OTRAG: Bold Pioneer Faces Hostile World" (PDF). L-5 News . Vol. 3, no. 2. L-5 Society. pp. 5–7. Archived from the original (PDF) on December 20, 2022. Retrieved December 20, 2022 via National Space Society.
  3. Leitenburger, Bernd. "OTRAG Rocket" . Retrieved December 20, 2022.
  4. Torchinsky, Jason (May 29, 2012). "SpaceX Was Not The First Private Rocket Company". www.jalopnik.com.
  5. "Space Transportation - Critical Newspaper Article on Shuttle Program". United States Department of State. 1976-07-06. Retrieved 2010-04-26.
  6. "Request for PL Export Transaction Check". United States Department of State. 1976-08-10. Retrieved 2010-04-26.
  7. Cohn, Stanley (April 1979). "What's Going Up in Zaire? OTRAG's Rocket Base in Shaba" (PDF). Munger Africana Library Notes. Pasadena, California: California Institute of Technology (49). ISSN   0047-8350 . Retrieved December 20, 2022.
  8. 1 2 Zuckerman, Ed (October 19, 1978). "Farms on the Asteroids: Hotels on the Moon". www.rollingstone.com.
  9. John Vinocur (1981-03-11). "Enigmatic West German Rocket Concern Finds A Home In Libyan Desert". The New York Times . Retrieved 2016-02-24.
  10. Wall, Kim (June 13, 2015). "Naked in an island idyll: eccentric couple recall a life of rockets and dictators". www.theguardian.com.
  11. 1 2 Astronautix.com OTRAG 2001 inc images
  12. "Core Management Team". Archived from the original on August 13, 2009. Retrieved August 9, 2009.
  13. "News Archive". Armadillo Aerospace. 2006-06-05. Archived from the original on 2016-03-03. Retrieved 2016-02-24.