DARE | |
Type | Student Team / Nonprofit |
Industry | Aerospace |
Founded | 2001 |
Headquarters | |
Products |
|
Services | Suborbital rocket launch, Research and Development |
Members | Est. 190+ (2020) |
Website | dare |
Footnotes /references [1] [2] |
Delft Aerospace Rocket Engineering is a student-run society within Delft University of Technology, with over 190 members. The main focus of the student group is the development of rocket technology on a non-profit basis. All development, from engines to electronics, is done in-house. Although several projects take place in DARE, the group's two flagship projects are Stratos and Project Sparrow. Stratos includes the Stratos I rocket which was launched in 2009 and set the European altitude record for amateur rocketry at 12.5 km. [3] [4] The follow-up of this rocket was the Stratos II+, which was launched on 16 October 2015, reaching an altitude of 21.5 km and breaking the European altitude record. [5] In summer of 2018, Stratos III was launched, disintegrating 20 seconds after the launch. Its successor, Stratos IV, was set to launch to 100 km, but never did due to ground systems failures during the launch campaign. Project Sparrow successfully developed a LOX/Ethanol, regeneratively cooled engine, and Stratos V, the latest flagship project, is building a reusable rocket around it. Even though DARE cooperates with the military to safely conduct launch campaigns, DARE's technology is strictly non-military. Approximately 70 percent of members come from the Faculty of Aerospace Engineering of Delft University of Technology, with the remaining 30% coming from other faculties, including Mechanical Engineering, Electrical Engineering, Applied Physics and Industrial Design. DARE also features a very high number of international students, with about half of the students coming from outside the Netherlands.
DARE was founded in 2001 by six students as a committee of the study association VSV Leonardo da Vinci of the Faculty of Aerospace Engineering on the TU Delft. The number of members has increased to over 190 in 2020. Over the years DARE has developed expertise in all three major rocket propulsion technologies (solid, liquid, and hybrid), with multiple conference papers published each year. 2009 marked DARE's Stratos I launch, which set the European altitude record of 12.5 km for student rockets. Afterwards, the development of Hybrid rocket engines was started, resulting in the 8 kN DHX-200 Aurora. This engine powered Stratos II, which after a failed launch campaign in 2014 broke the European altitude record for student rocketry in 2015.
DARE typically conducts two to four launch days each year for small scale rockets that go up to a maximum of two kilometers altitude. These launches take place on a military site near 't Harde in the North of the Netherlands. To go to higher altitudes, DARE occasionally participates in launch campaigns elsewhere in Europe.
The work of DARE takes place at two locations at the TU Delft campus. The first is a manufacturing-orientated workshop in the faculty of Aerospace Engineering's Aircraft Hall. Here, the major parts of rocket production take place, from machining of metallic parts to soldering electronics boards. The other location is the Science Center Delft, where meetings and lectures from more experienced members take place.
DARE has a number of teams working on specific areas of rocket technology, logistics, promotion and sponsor acquisition.
Most rockets of DARE run on solid propellant engines, which are developed and built by the Solid Six team and the Safety Board. The propellants used is either a mixture of sorbitol and potassium nitrate, known as rocket candy, or a mixture of Ammonium Nitrate and Aluminium called Alan-7. The scale of the developed engines ranges from 300 N up to 7000 N.
After the launch of Stratos I, research to Hybrid rocket engines started within DARE. After extensive theoretical research, small scale testing (ranging from 500 to 1100 N) commenced to gain experience with the system and to select the optimal engine configuration. The selected fuel was a mixture of Sorbitol, Paraffin and Aluminium, combined with Nitrous Oxide as oxidizer. This work has resulted in several publications in several different journals including the journal of the American Institute of Aeronautics and Astronautics. [6] Scaled-up versions of this engine are used to power Stratos II+ and III, the flagship projects of DARE.
While currently all large-scale engines developed by DARE are Nitrous Oxide - based Hybrid engines, logistics and manufacturing prevents this type of engine to be scaled up much further. For this reason, the development of LOX - Ethanol Liquid rocket engines is tackled within DARE. Past liquid engine developments have failed for a variety of reasons, but most prominently due to the mechanical complexity of this type of propulsion. The Cryogenic Engine Development subdivision of DARE aims to produce a 2-3 kN engine, to acquire the knowledge required for the society to tap into the technology. A future plan for this engine is potentially powering future Stratos missions.
All DARE rockets are passively stabilised, with fin size and -location balanced such that the rocket turns into the wind once it clears the tower. As a consequence, medium to high crosswinds can severely limit the altitude a rocket can achieve. The Advanced Control Team is developing technology to actively stabilize the rocket during ascend.
All PCB's and software are custom-made and developed in-house within DARE. They are used to deploy parachutes, control engines, and transmit radio data during and after launch.
The Small Rocket Project (colloquially known as the Scrambled Eggs Competition) is DARE's program to introduce first year members and other interested students to the basic principles of hands-on rocketry. The aim of the project is to launch a rocket to an altitude of 1 km with an uncooked egg on board and returning this egg intact. To help students achieve this goal the project starts out with several lectures explaining the fundamentals of rocketry, rocket stability and the design of parachutes. These lectures are given by senior DARE members, who are also mentors that advise and guide the groups during the project. The groups are largely free in their designs, although every rocket has to pass a final safety check, and the solid rocket motors for the rockets are provided by DARE. The project concludes with a launch day at a military testing range, where each design is put to the test.
DARE is also actively involved in providing the launch service for the Dutch CanSat project. [7] In particular, DARE develops, produces, tests, and launches the CanSat launchers (CSL). Over the years these launcher have undergone several development iterations, balancing reliability, producibility, and payload capacity. The current CSL Version 7 consists of an all-Aluminium frame and, propelled by a solid rocket motor, can lift about five to six CanSats to an altitude of one kilometer. The CSL V7 has recently been used as a flying testbed to test new technologies developed by DARE.
In 2015, the Aether project was kicked off. It focusses on demonstrating several new technologies developed within DARE, that can later on be implemented in larger projects. It includes:
The Safety Board does not actively develop rockets, but consists of experienced DARE members, that can join the Safety Board after a minimum of one-year training. [8] The Safety Board oversees testing done in DARE, checks rockets prior to launch, and is responsible for all safety-related elements of DARE's work. The Safety Board can overrule any safety-related decision.
Project Sparrow is the newest initiative of DARE, towards building the society’s first liquid-propelled, thrust-vectoring rocket engine, which will be named Firebolt. It shall provide the required power and control using a LOX – Ethanol engine, to build rockets that go beyond the 100 km Kármán line. This engine will be the successor to the hybrid-powered Nimbus used in the DARE Stratos IV rocket, powering DARE’s next generation of high-performance rockets, and will be the first step towards sending the first student-designed rocket into orbit around Earth.
Project Sparrow will eventually develop a flight-ready engine, which could be integrated by DARE into a sounding rocket; the sounding rocket will also be a testbed for validating rocket dynamics with the thrust-vectoring engine. The rocket eventually will incorporate staging and recovery systems.
Stratos I set the record for the highest altitude achieved by a student rocket, at 12.5 km. [9] It was launched from Esrange in Sweden in 2009. It was a two-staged solid rocket, powered by boosters developed and built within DARE. After a successful ascent, the parachutes failed to deploy and both stages crashed. The achieved altitude and the crash location could be gathered from the launch range equipment, making it possible to retrieve the second stage after the launch. The first stage was only accidentally found back 8 years later, during a routine check of the launch site.
Function | Sounding Rocket |
---|---|
Manufacturer | DARE |
Country of origin | Netherlands |
Size | |
Height | 6.9 m (23 ft) |
Diameter | 20 cm (7.9 in) |
Mass | 185 kg (408 lb) |
Stages | 1 |
Launch history | |
Launch sites | El Arenosillo |
Boosters – DHX-200 Aurora | |
Maximum thrust | 11 kN (peak) |
Specific impulse | 205 s |
Burn time | 23 |
Propellant | Sorbitol, Paraffin, Aluminium / Nitrous oxide |
The Stratos II+ rocket was DARE's biggest undertaking and originally aimed to reach 50 km. However after design changes and updated simulations it became unlikely that this altitude could be reached. Stratos II+ was successfully launched on 16 October 2015 from El Arenosillo of Instituto Nacional de Técnica Aeroespacial, close to the city of Sevilla in Spain. It reached an altitude of 21.5 km, with which it broke the previous record for student rocketry. [10] The rocket was initially known as the Stratos II but failed to launch in October 2014. Design improvements were made after which the rocket was named Stratos II+.
Stratos II+ was powered by a single-stage hybrid engine, the DHX-200 Aurora which has a peak output of 11 kN. The engine has a total impulse of 180 kNs and burns for approximately 23 seconds. [11] After this the engine is cut and the rocket continued on coast to its apogee. Stratos II+ carried several scientific payloads on board to do measurements in the higher atmosphere. Among these are an experiment on radio astronomy from the Radboud University Nijmegen, [12] a camera system with video link from the company DelftDynamics [13] [14] and a geiger counter from the Hungarian Academy of Sciences' Centre for Energy research.
An overview of the launch attempts of Stratos II and II+ is shown in the table below.
Attempt | Planned | Result | Turnaround | Reason | Decision point | Weather go (%) | Notes |
---|---|---|---|---|---|---|---|
1 | 1 Oct 2014, 11:00:00 am | scrubbed | — | Weather | |||
2 | 2 Oct 2014, 6:15:00 pm | scrubbed | 1 day, 7 hours, 15 minutes | Flight Termination System failure | (T-1:20) | ||
3 | 3 Oct 2014, 3:15:00 pm | scrubbed | 0 days, 21 hours, 0 minutes | Main oxidizer valve stuck as by-effect of leaking N2O from the feed system | (T-0:01) | ||
4 | 15 Oct 2015, 4:00:00 pm | scrubbed | 377 days, 0 hours, 45 minutes | Igniter valve did not open resulting in failed ignition | 100 | ||
5 | 16 Oct 2015, 4:33:00 pm | success | 1 day, 0 hours, 33 minutes | - | 100 | Apogee altitude of 21.5 km |
Function | Sounding Rocket |
---|---|
Manufacturer | DARE |
Country of origin | Netherlands |
Size | |
Height | 8.2 m (27 ft) |
Diameter | 28 cm (11 in) |
Mass | 330 kg (730 lb) |
Stages | 1 |
Launch history | |
Launch sites | El Arenosillo |
Boosters – DHX-400 Nimbus | |
Maximum thrust | 25 kN (peak) |
Specific impulse | 179 s |
Propellant | Sorbitol, Paraffin, Aluminium / Nitrous oxide |
Stratos III is an expendable sounding rocket developed by the student rocketry team Delft Aerospace Rocket Engineering of the TU Delft. The project started in 2016 as a successor of the Stratos II+ mission with the purpose of reclaiming the European altitude record for student rocketry, currently owned by the German team HyEnD.
The Stratos III rocket is 8.2 m tall and is powered by the DHX-400 Nimbus, a 360 kNs impulse hybrid rocket engine. [15] The DHX-400 Nimbus utilizes nitrous oxide as its oxidizer and a mixture of paraffin, sorbitol and aluminum powder for the fuel. The oxidizer tank is made out of carbon fiber with an aluminium liner and is capable of storing 174 kg of nitrous oxide at a pressure of 60 bar. The DHX-400 is the most powerful amateur built hybrid engine in the world, with a peak thrust of 25 kN. [16]
The rocket carries a scientific payload from NLR, which is a prototype IMU for the proposed future European SMILE launcher. [17] Additionally Stratos III has full 360 degree live stream downlink.
At apogee the nosecone with payload separates from the oxidizer tank and propulsion system. After this a parachute deployment device opens a drogue parachute and main parachute to ensure a safe landing of 13 m/s in the Atlantic Ocean. After this, the nosecone is recovered by a boat. Stratos III is launched from El Arenosillo, similar to Stratos II+. The launch window opens at July 16, 2018 and closes at July 27, 2018. An overview of the launch attempts is shown in the table below.
Attempt | Planned | Result | Turnaround | Reason | Decision point | Weather go (%) | Notes |
---|---|---|---|---|---|---|---|
1 | 24 Jul 2018, 9:00:00 pm | cancelled | — | winds too strong | (T-2:50) | 25 | |
2 | 26 Jul 2018, 3:30:00 am | failure | 1 day, 6 hours, 30 minutes | loss of vehicle 20 seconds into the flight | (T+0:20) | 100 |
The second launch attempt was initially scheduled for July 25 at 11 PM CEST. However, with a 100% weather-GO, a significant delay occurred when pressurizing the nitrous oxide tank. This led to the launch being delayed to July 26 3:30 AM. After a successful launch, an anomaly occurred 20 seconds into the flight, resulting in a loss of the vehicle. [18]
Function | Sounding Rocket |
---|---|
Manufacturer | DARE |
Country of origin | Netherlands |
Size | |
Height | 8.3 m (27 ft) |
Diameter | 28 cm (11 in) |
Mass | 320 kg (710 lb) |
Stages | 1 |
Boosters – DHX-400 Nimbus | |
Maximum thrust | 26 kN (peak) |
Specific impulse | 179 s |
Propellant | Sorbitol, Paraffin, Aluminium / Nitrous oxide |
After the in-flight disintegration of Stratos III, an investigation was begun to determine the cause of the vehicles demise. The team behind the investigation consisted of members of the Stratos III team as well as the newly formed Stratos IV team. The main sources of information were the telemetry streamed back from the vehicle during its 20 seconds of flight (giving data from the two IMUs onboard as well as the GPS receiver and pressure sensors), as well as the ground measurements taken using radar and Doppler. These sources allowed the team to piece together a picture of the path Stratos III followed during its flight. From this data it was concluded that the vehicle underwent a phenomenon known as roll-pitch coupling, or inertia coupling. This occurs when the vehicles roll rate matches the natural pitch frequency of the vehicle. This causes the vehicle to move in a conical motion rather than a linear motion, and when the two frequencies couple, the vehicle becomes unstable and diverges from its flight path, causing it to break up.
When the goal of Stratos IV was considered, the engine performance/vehicle mass combination of Stratos III bore a large influence. This combination was seen to give simulated apogees approaching 100 km, or the Karman line. As reaching this altitude is the long term goal of the Stratos project, it was decided to iterate upon the design of Stratos III. Thus the Stratos IV project is focusing on minimizing the mass of the vehicle, while keeping the internal engine geometry, which took three years to develop, fixed. The design of Stratos IV was unveiled on February 12, 2019. [19]
The design changes in comparison to Stratos III are:
The Stratos IV launch campaign was held in late 2021 at the El Arenosillo Test center. [20] After technical issues on several attempts, the rocket was not launched and the campaign ended. [21]
A rocket is a vehicle that uses jet propulsion to accelerate without using the surrounding air. A rocket engine produces thrust by reaction to exhaust expelled at high speed. Rocket engines work entirely from propellant carried within the vehicle; therefore a rocket can fly in the vacuum of space. Rockets work more efficiently in a vacuum and incur a loss of thrust due to the opposing pressure of the atmosphere.
A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer). The earliest rockets were solid-fuel rockets powered by gunpowder; they were used in warfare by the Chinese, Indians, Mongols and Persians as early as the 13th century.
A hybrid-propellant rocket is a rocket with a rocket motor that uses rocket propellants in two different phases: one solid and the other either gas or liquid. The hybrid rocket concept can be traced back to the early 1930s.
A model rocket is a small rocket designed to reach low altitudes and be recovered by a variety of means.
A sounding rocket or rocketsonde, sometimes called a research rocket or a suborbital rocket, is an instrument-carrying rocket designed to take measurements and perform scientific experiments during its sub-orbital flight. The rockets are used to launch instruments from 48 to 145 km above the surface of the Earth, the altitude generally between weather balloons and satellites; the maximum altitude for balloons is about 40 km and the minimum for satellites is approximately 121 km. Certain sounding rockets have an apogee between 1,000 and 1,500 km, such as the Black Brant X and XII, which is the maximum apogee of their class. Sounding rockets often use military surplus rocket motors. NASA routinely flies the Terrier Mk 70 boosted Improved Orion, lifting 270–450-kg (600–1,000-pound) payloads into the exoatmospheric region between 97 and 201 km.
High-power rocketry is a hobby similar to model rocketry. The major difference is that higher impulse range motors are used. The National Fire Protection Association (NFPA) definition of a high-power rocket is one that has a total weight of more than 1,500 grams (3.3 lb) and contains a motor or motors containing more than 125 grams (4.4 oz) of propellant and/or rated at more than 160 Newton-seconds of total impulse, or that uses a motor with an average thrust of 80 newtons (18 lbf) or more.
The Korea Aerospace Research Institute (KARI), established in 1989, is the aeronautics and space agency of South Korea. Its main laboratories are located in Daejeon, in the Daedeok Science Town. KARI's vision is to continue building upon indigenous launch capabilities, strengthen national safety and public service, industrialize satellite information and applications technology, explore the Moon, and develop environmentally-friendly and highly-efficient cutting-edge aircraft and core aerospace technology. Current projects include the KSLV-2 launcher. Past projects include the 1999 Arirang-1 satellite. The agency was founded in 1989. Prior to South Korea's entry into the Institute for Advanced Engineering (IAE) in 1992, it focused primarily on aerospace technology.
The Australian Space Research Institute (ASRI) was formed 1991 with the merger of the AUSROC Launch Vehicle Development Group at Monash University, Melbourne and the Australian Space Engineering Research Association (ASERA).
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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.
El Arenosillo Test Centre (CEDEA) is the name of a rocket launch site for suborbital rockets managed by INTA, located near Mazagón in Spain. It is located in the province of Huelva, Andalucía, in the southwest coast of Spain (37.1° N, 6.7° W). CEDEA is adjacent to the Center of Excellence for Unmanned Systems (CEUS).
RocketMotorTwo (RM2) is a family of hybrid rocket engines developed for the Scaled Composites SpaceShipTwo suborbital spaceplane.
Nitrous oxide fuel blend propellants are a class of liquid rocket propellants that were intended in the early 2010s to be able to replace hydrazine as the standard storable rocket propellent in some applications.
Rocket propellant is the reaction mass of a rocket. This reaction mass is ejected at the highest achievable velocity from a rocket engine to produce thrust. The energy required can either come from the propellants themselves, as with a chemical rocket, or from an external source, as with ion engines.
The Advanced Rocket Research Center is a Taiwanese space transport research organization headquartered at National Chiao Tung University in Hsinchu City, Taiwan, with a research focus in hybrid rockets. Founded in April 2012, ARRC is supported by research grants and private donors through crowdsourcing platforms.
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The Scientific Workgroup for Rocketry and Spaceflight (WARR) is a scientific workgroup situated at Technical University of Munich, composed mainly of its students. It was founded by students in 1962 with the goal to compensate for the lack of a chair for space technology at the university at the time. Since the establishment of such a chair in 1966, the group has conducted practical projects, starting with the first successful development and of a hybrid rocket in Germany. One rocket of this type was launched in 1972, another is on permanent display at Deutsches Museum. WARR has attained some public attention by for its projects in space elevator competitions, small satellites interstellar spaceflight concepts, and for winning all SpaceX Hyperloop pod competitions.
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The Kuwait Space Rocket (KSR), is a Kuwaiti project to build and launch the first suborbital liquid bi-propellant rocket in Arabia. The project is intended to be the first step towards starting a space industry in the country and a launch service provider in the GCC region. The project is divided into two phases with two separate vehicles. An initial testing phase with KSR-1 as a test vehicle capable of reaching an altitude of 8 km (5.0 mi) and a more expansive suborbital test phase with the KSR-2 planned to fly to an altitude of 100 km (62 mi). in May 16 Ambition-1 launched but had a malfunction with the parachute and crashed in free fall.
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