Sharp Edge Flight Experiment
SHEFEX (Sharp Edge Flight Experiment), is an experiment conducted by the German Aerospace Center (DLR), for the development of some new, cheaper and safer design principles for space capsules, hypersonic vehicles and spaceplanes with re-entry capability in the atmosphere and their integration into a complete system.
DLR explained the objectives of SHEFEX: The aim of the research is a spaceplane that is usable for experiments under microgravity from 2020 on.[1] It is set to finish with a space plane project named REX Freeflyer(REX for Returnable experiment, dt. Rückkehrexperiment).[2]
During re-entry of spacecraft into the earth's atmosphere, the high velocity of the spacecraft together with friction and displacement of air molecules leads to temperatures of over 2000 °C.[1] In order to not burn up, spaceships need very expensive and sometimes failing heat shields.
Contents
First spacecraft with sharp corners and edges
The namesake idea for the sharp-edged flight experiment of Hendrik Weihs, coordinator for returning technologies DLR, is an entirely new form for a spacecraft, namely with sharp corners and edges instead of the rounded shapes ubiquitously used in space flight today. Few flat tile shapes can be produced at lower cost than highly individual rounded shapes.[1]
Dr. Klaus Hannemann, Head of the spacecraft department at the DLR Institute of Aerodynamics and Flow Technology in Göttingen explains the fundamental advantage of the concept:
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Additionally, the project is aimed at improving aerodynamics. General Project Manager Hendrik Weihs said:
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Programmatically, the DLR, said:
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SHEFEX I
SHEFEX I was the first experimental vehicle of the SHEFEX project[4] and launched on Thursday, 27 October 2005 from the Andøya Rocket Range in Norway. Shefex I reached a height of about 200 km over the North Sea. Within 20 seconds, the vehicle re-entered Earth's atmosphere at almost seven times the speed of sound. The measured data and live images of the on-board camera were transferred directly to the ground station. However, during the activation of the parachute system an error occurred that led to the loss of the parachute system and consequently to the loss of the flight unit. According to the DLR, the evaluation of the data provided important insights so that SHEFEX I could be seen as a great success from the perspective of the DLR. For the flight, a missile system was used, which consisted of a combined Brazilian VS-30 lower level and a HAWK rocket as the second stage. The cost of the three-year project was approximately 4 million euros. It was part of the space program of the Helmholtz Association of German Research Centers (HGF) and the DLR.
SHEFEX II
With SHEFEX II, nine different thermal protection systems were to be evaluated on the facetted skin, mainly new fiber ceramics. Additionally, the aerospace companies EADS Astrium and MT Aerospace as well as Boeing used some of the surface of SHEFEX II for their own experiments. The vehicle was equipped with sensors to measure pressure, heat flux, and temperature in the vehicle tip.
On 22 June 2012, SHEFEX II was launched from the same launch station, the Andøya Rocket Range in Norway. It reached a height of about 180 kilometers and a speed of about 11,000 kilometers per hour (eleven times the speed of sound). The rocket used was the Brazilian VS-40. During its re-entry, SHEFEX II survived temperatures above 2500 °C, while sending data from the 300 different sensors to the ground station.
SHEFEX III
For 2016 the DLR plans SHEFEX III, a spaceplane-like vehicle. It should fly even faster and stay in the air for 15 minutes, far longer than the previous two experiments.[5]
REX Free Flyer (SHEFEX IV)
The REX-Free Flyer is planned as a first application of the experience collected from SHEFEX. This system should serve as a free-flying platform for high quality microgravity experiments over several days. The possibility of controlled return and a modular design of the experiment trays, that closely resemble those found on sounding rockets, should give experimenters quick and inexpensive access to their experiments.[6]
References
- ↑ 1.0 1.1 1.2 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Seite des Institut für Bauweisen- und Konstruktionsforschungder DLR über das Projekt REX-Free Flyer, Retrieved 2012-06-28
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ DLR/Redaktion Astronews.com: SHEFEX II. Erfolgreicher Testflug lieferte wichtige Daten. Retrieved 2012-06-29
- ↑ DLR-Handout: SHEFEX II Ein weiterer Schritt im Flugtestprogramm für Wiedereintrittstechnologie PDF file
