Wednesday, April 17, 2013

NASA looks to 3D printing for space exploration

NASA looks to 3D printing for space exploration
3ders.org, 17 April 2013
http://www.3ders.org/articles/20130417-nasa-looks-to-3d-printing-for-space-exploration.html

3D printing, as one innovative technology will help us advance the future of manufacturing. At NASA, the revolution is already under way. At the NASA's Marshall Space Flight Center additive manufacturing is used to create parts for a next-generation rocket that will launch astronauts to the most distant destinations ever.

Monday, April 15, 2013

New F-1B rocket engine

New F-1B rocket engine
Ars Technica, 15 April 2013
http://arstechnica.com/science/2013/04/new-f-1b-rocket-engine-upgrades-apollo-era-deisgn-with-1-8m-lbs-of-thrust/

NASA has spent a lot of time and money resurrecting the F-1 rocket engine that powered the Saturn V back in the 1960s and 1970s, and Ars recently spent a week at the Marshall Space Flight Center in Huntsville, Alabama, to get the inside scoop on how the effort came to be. But there's a very practical reason why NASA is putting old rocket parts up on a test stand and firing them off: its latest launch vehicle might be powered by engines that look, sound, and work a whole lot like the legendary F-1.

Sunday, April 14, 2013

How NASA brought the monstrous F-1 “moon rocket” engine back to life

How NASA brought the monstrous F-1 “moon rocket” engine back to life
Ars Technica, 15 April 2013
http://arstechnica.com/science/2013/04/how-nasa-brought-the-monstrous-f-1-moon-rocket-back-to-life/

There has never been anything like the Saturn V, the launch vehicle that powered the United States past the Soviet Union to a series of manned lunar landings in the late 1960s and early 1970s. The rocket redefined "massive," standing 363 feet (110 meters) in height and producing a ludicrous 7.68 million pounds (34 meganewtons) of thrust from the five monstrous, kerosene-gulping Rocketdyne F-1 rocket engines that made up its first stage.

Sunday, April 7, 2013

Online: Nozzle Theory

Flow Processes in Rocket Engines Nozzles with Focus on Flow Separation and Side-Loads
Swedish Royal Institute of Technology, 2002
www.mech.kth.se/thesis/2002/lic/lic_2002_jan_ostlund.pdf

The present thesis presents a comprehensive, up-to-date review of supersonic flow separation and side-loads in internal nozzle flows with ensuing side-loads. In addition to results available in the literature, it also contains previously unpublished material based on this author’s work, whose main contributions are

  1. discovery the role of transition between different separation patterns for side-load generation
  2. experimental verification of side-loads due to aeroelastic effects and
  3. contributions to the analysis and scaling of side-loads.

Thursday, April 4, 2013

NASA selects small businesses to build nanosatellite launchers

NASA selects small businesses to build nanosatellite launchers
Flight Global, 4 April 2013
http://www.flightglobal.com/news/articles/nasa-selects-small-businesses-to-build-nanosatellite-launchers-384221/

NASA has selected small businesses to receive up to $38.7 million in grants for innovative technology developments, including a number of technologies relating to nanosatellite launch vehicles.

Wednesday, April 3, 2013

Ionic Wind Thrusters Demonstrate High Efficiency

A mighty wind
MIT News, 3 April 2013
http://web.mit.edu/newsoffice/2013/ionic-thrusters-0403.html

Now researchers at MIT have run their own experiments and found that ionic thrusters may be a far more efficient source of propulsion than conventional jet engines. In their experiments, they found that ionic wind produces 110 newtons of thrust per kilowatt, compared with a jet engine’s 2 newtons per kilowatt. The team has published its results in the Proceedings of the Royal Society.

Also see: Performance Characterization of Electrohydrodynamic Propulsion Devices.