|
|
SpaceShip 1, 2 ..n by
[email protected]
A lot of discussion on this and other groups orbits around
the difficulty is scaling SS1 to an orbital vehicle.
There has been a lot of discussion about Mr...
|
|
6 |
1,231 |
|
|
A vision of CATS by
Penguinista
Presuming a reusable spacecraft
- Have to avoid armies of technicians to operate/maintain the
spacecraft. Thus:
- Components must have an appreciable...
|
|
5 |
1,422 |
|
|
engine construction by
Penguinista
Reading about the conventional bundled tube regenerative cooling chamber
is made, it sounds laborious, and with so many little parts to get wrong.
I was...
|
|
2 |
1,183 |
|
|
feedback on orbiter concept? by
Penguinista
http://splitreflection.com/cal/shuttle.png
A simple shuttle orbiter concept I've drawn up based on certain princibles.
- This would be an upper stage, though...
|
|
2 |
1,459 |
|
|
n2o, ethane, co2 ethene mixtures by
Penguinista
toby peers wrote:
Sometimes people on this group have mentioned mixed liquid monprops
like methane and oxygen and that they are very dangerous. What
...
|
|
2 |
1,179 |
|
|
reentry with edges transverse to flow? by
Penguinista
I'm thinking a shape like a sharp edged saucer doing reentry face first
and then turning edge on for low speed landing. I expect some
concentration of heating...
|
|
1 |
1,143 |
|
|
Pulse Jets by
pervect
A week or so ago I saw a rather neat Junkyard Wars episode on
pulse-jets. I'm also rather intrigued that it was felt to be a safe
enough gadget to build for...
( 1 2 3 ... Last Page)
|
|
61 |
5,327 |
|
|
|
|
16 |
1,057 |
|
|
Orbiting fuel depot concept by
Peter Fairbrother
Derek Lyons wrote:
Peter Fairbrother wrote:
Derek Lyons wrote:
Peter Fairbrother wrote:
...
|
|
3 |
949 |
|
|
Silver plating by
Peter Fairbrother
Tom wrote:
So how big is the impellor going to be in this pump?
It doesn't have one.
I considered a volute casing Barske-type impellor pump, but it would...
|
|
3 |
590 |
|
|
Polythene tanks? by
Peter Fairbrother
Reading the thread about cryogenic plastics, I thought it might be an idea
to use (reinforced? with what?) polythene for the tanks of my LH2/LOX second
stage*...
( 1 2 3 ... Last Page)
|
|
35 |
1,565 |
|
|
Mars sample return by
Peter Fairbrother
Suppose we want to bring a small sample back from Mars. The Mars rovers mass
around 180 kg. If 10% was reserved for the return rocket it would mass 18
kg.
We...
|
|
3 |
935 |
|
|
A new planet? by
Peter Fairbrother
Suppose you joined Mars and Venus together with a big elastic band?
--
Peter Fairbrother
|
|
6 |
1,468 |
|
|
Rockets of ice? (ALICE) by
Peter Stickney[_2_]
Jim Davis wrote:
Derek Lyons wrote:
There was a guy I saw somewhere recently who was seriously
proposing to save on booster weight by using a fuel...
|
|
0 |
830 |
|
|
Mars rover tracks? by
Peter Trei
Looking at the Mars Rover tracks, I notice that at
regular intervals a few feet apart, the treadmarks
left in the dust are disturbed for a few inches...
|
|
9 |
1,073 |
|
|
|
|
1 |
596 |
|
|
Future of the RL60? by
Phil Paisley
Is the RL60 a 'done deal' for some variants of the Delta 4 and Atlas
5? If so what effects will it have on payloads - presumably to GTO
but also on...
|
|
8 |
861 |
|
|
"Off the shelf" heavy lift??? by
Phil Paisley
Take 2 Shuttle SRBs, possibly the 5 segment ones that were just
tested. Hang a Delta 4 core between them (gonna look odd, but no
odder than a Titan 4). ...
|
November 23rd 03 06:49 AM
by Treez03
|
3 |
2,025 |
|
|
Back to the moon, only CEV reuseable? by
Philip
Looking at the planned vehicles for the return to the moon, the
article(s) seemed to emphasize leverage of shuttle technology. For
example the use of SSMEs and...
|
|
5 |
813 |
|
|
Aerospikes by
Proponent
Bono's aerospike designs from the 60s feature toroidal comubstion
chambers, whereas recent designs like the X-33's linear aerospike
usually have several small,...
|
|
1 |
665 |