| Thread | Last Post | Replies |
|
| Spaceshipone high altitude nozzle missing | 28 Apr 2004 17:59 GMT | 4 |
Did anyone notice that the high altitude nozzle extension seems to be attached when first fired but does not seem to be there later? The picks at scaled.com show the large black extension at first but after burnout it is gone (2nd powered flight). The best
|
| Venusian rocketry. | 28 Apr 2004 12:22 GMT | 4 |
Can practical rocketry be done on the venusian surface, or is it basically out of the question. Might things like ejector ramjets be very efficient?
|
| Long baseline optical interferometer | 28 Apr 2004 03:17 GMT | 2 |
Could Hubble, along with the NexGen space telescope operate as a long baseline optical interferometer in some way? Perhaps a reference laser beam could be sent from one telescope to the other. Any potential advantages in using adaptive optic methods whereby a
|
| Uprated, near-term fiction capsules | 27 Apr 2004 16:04 GMT | 4 |
I'm trying to spec out a capsule-based launch system for some stories I've been writing. One of my goals with this project is to be as technically realistic as possible. The main components are 3 and 10-seat capsules, loosely based on
|
| Please help me ID what I saw on Discovery Wings | 27 Apr 2004 03:34 GMT | 18 |
I am going to describe something I saw on Discovery Wings and I hope you can help identify it. It was footage of an experiment that was not fully described in the story on use of satellites to assist allied soldiers in wartime.
|
| SSTO propulsion overview | 19 Apr 2004 04:10 GMT | 68 |
Catching up on some unread journals, I note that the March/April 2003 issue of JBIS has a very interesting paper: "A comparison of propulsion concepts for SSTO reusable launchers", by Richard Varvill and Alan Bond. While the authors have a mild case of hydrogen religion -- ...
|
| Shuttle based lunar vehicle | 17 Apr 2004 10:13 GMT | 3 |
I have a feeling that now that we have had a couple of shuttle accidents we are moving away from the shuttle too eagerly. If I had to go to the Moon today, I would try to work as much as possible with the systems we have, like for example the shuttle.
|
| Starpower? | 17 Apr 2004 06:57 GMT | 3 |
The ultimate in solar collectors must be the deposition of solar collectors onto the solar surface. The sun puts out 3.86x10^26 watts of power. Distributed over a sphere whose radius is equal to the radius of Earth's orbit this falls to a little less than 1,400 watts
|
| SpaceShipOne 2nd Powered Flight | 15 Apr 2004 02:58 GMT | 3 |
So according to early reports, SpaceShipOne made its second powered flight reaching Mach 2, only a day after Scaled was granted a suborbital launch license by the FAA. Although the license allows the vehicle to travel above 60 miles, this test flight went to 105,000
|
| Possible solution for Hubble? | 09 Apr 2004 13:56 GMT | 2 |
http://www.spacedaily.com/news/salvage-04a.html Could this possibly be used to bring the Hubble to the ISS for repairs?
|
| Tell me about the LEM | 09 Apr 2004 09:33 GMT | 5 |
The Lunar Lander has always fascinated me. The first (and only) manned spacecraft to land on another world. Not being a part of that part of history,
|
| Re: How much more efficient would Nuclear Fission rockets be? | 09 Apr 2004 08:12 GMT | 3 |
"Ian Stirling" <root@mauve.demon.co.uk> wrote in message news:4OG8c.23859$h44.3117758@stones.force9.net...
> Christopher M. Jones <vegemite@dualboot.net> wrote: > > "Rats" <rubix@chump.com> wrote in message |
| Beamed power to space vehicles | 06 Apr 2004 22:05 GMT | 1 |
What is the maximum flux levels that can be beamed to space craft by lasr or microwave? The specific application would be to beam power from a SSPS (power available: 5GW) to a space vehicle using an electric drive (e.g.
|
| Lunar Transport System Components | 06 Apr 2004 04:34 GMT | 12 |
What components need to make up the lunar transport architecture? One thing I'm not too sure of is the difference between OSP and CEV. Is CEV just be an enhancement of OSP? Assuming we rely on the current range of heavy launchers like Delta IV
|