Re: [ERPS] KISS III Propulsion System Test

2002-11-02 Thread Randall Clague
On Sat, 02 Nov 2002 04:45:15 +, Ian Woollard <[EMAIL PROTECTED]> wrote: >But then I realised you could carry a COaxial Resealing Kit to manually >seal this off . That would work. Or maybe a Big UNiversal Gasket could >be used. Hmm. Perhaps I should patent this idea quickly before someone >

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Ian Woollard
Hmm. Have visions of this hand-operated valve getting stuck and everyone gasping their last. That's bad. But then I realised you could carry a COaxial Resealing Kit to manually seal this off . That would work. Or maybe a Big UNiversal  Gasket could be used. Hmm. Perhaps I should

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Randall Clague
On Sat, 2 Nov 2002 10:13:44 +1100, "Jake Anderson" <[EMAIL PROTECTED]> wrote: >I am just struck by the similarity between what is happening now and the >mercury 7 sub-orbital flight And that just chased away my cynical pessimism. Thank you, Jake. The key part of your observation is exactly that

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Randall Clague
On Fri, 01 Nov 2002 17:05:00 -0600, John Carmack <[EMAIL PROTECTED]> wrote: >Our current thinking is to carry an air bottle, and intentionally let the >cabin leak a bit to force some air circulation, dehumidification, and >cooling. There will also be a hand-operated valve to force it to leak mo

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Jake Anderson
- Original Message - From: "John Carmack" <[EMAIL PROTECTED]> To: <[EMAIL PROTECTED]> Sent: Saturday, November 02, 2002 10:05 AM Subject: Re: [ERPS] KISS III Propulsion System Test > > > > >We ran a similar exercise here for Armadillo's life suppor

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread John Carmack
At 09:26 AM 11/1/2002 -0800, you wrote: On Fri, 01 Nov 2002 08:16:06 -0800, Doug Jones <[EMAIL PROTECTED]> wrote: >I kinda get the impression that once the cat bed is warmed by a previous >pulse, subsequent ones should not have significant uncatalyzed >throughput, and PWM throttling keeps the bed

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread John Carmack
We ran a similar exercise here for Armadillo's life support system. We concluded that they didn't need one. The flight is so short, and the cabin so large, that CO2 levels won't rise to uncomfortable levels during the flight even if they don't scrub the air. We also determined that dumping the

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Randall Clague
On Fri, 01 Nov 2002 08:16:06 -0800, Doug Jones <[EMAIL PROTECTED]> wrote: >I kinda get the impression that once the cat bed is warmed by a previous >pulse, subsequent ones should not have significant uncatalyzed >throughput, and PWM throttling keeps the bed hot. Good point. If we can assume th

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Randall Clague
On Fri, 01 Nov 2002 14:31:35 +, Ian Woollard <[EMAIL PROTECTED]> wrote: >>Where do you imagine we'll fly POGO that's cold enough to matter? >> >Hmm. I haven't checked but I would expect launch licenses would be >easier to get near Ottawa or Toronto ;-) > >You'd have difficulty getting an expo

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Randall Clague
On Fri, 1 Nov 2002 08:03:45 -0500, "Sean Patrick Daly" <[EMAIL PROTECTED]> wrote: >I don't know about anyone else, but I'm under the impression that the higher >you go, the colder you get. So I guess the real question is... What is going >to happen to the H2O2 above say... 50,000+ feet? Will the e

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Doug Jones
Randall Clague wrote: On Thu, 31 Oct 2002 23:53:58 -0800, <[EMAIL PROTECTED]> wrote: Tape heaters are inappropriate for Spike, since the propellant tank is part of the aeroshell and it needs to be very clean aerodynamically Hm, I'd been assuming the tanks were not integral. If they are, the

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Ian Woollard
Randall Clague wrote: On Thu, 31 Oct 2002 23:53:58 -0800, <[EMAIL PROTECTED]> wrote: Where do you imagine we'll fly POGO that's cold enough to matter? Hmm. I haven't checked but I would expect launch licenses would be easier to get near Ottawa or Toronto ;-) You'd have difficulty getting

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Jake Anderson
warm-up time - Original Message - From: "Randall Clague" <[EMAIL PROTECTED]> To: "ERPS" <[EMAIL PROTECTED]> Sent: Friday, November 01, 2002 7:51 PM Subject: Re: [ERPS] KISS III Propulsion System Test > On Fri, 1 Nov 2002 18:45:05 +1100, "Ja

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread eric
On 1 Nov, Randall Clague wrote: > If you fly the heater - really just some resistive tape wrapped around > the tank - then the only moving part you have to worry about for > pre-liftoff heater disconnect is the power plug. I dislike moving > things around just prior to liftoff, but I can live wit

RE: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Sean Patrick Daly
us 100F for a while. Anyone have any data on that? Sean -Original Message- From: [EMAIL PROTECTED] [mailto:erps-list-admin@;lists.erps.org]On Behalf Of Jake Anderson Sent: Friday, November 01, 2002 2:45 AM To: ERPS Subject: Re: [ERPS] KISS III Propulsion System Test why fly t

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Randall Clague
On Thu, 31 Oct 2002 23:53:58 -0800, <[EMAIL PROTECTED]> wrote: >Tape heaters are inappropriate for Spike, since the propellant tank is part of >the aeroshell and it needs to be very clean aerodynamically Hm, I'd been assuming the tanks were not integral. If they are, then tape heaters get margin

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Randall Clague
On Fri, 1 Nov 2002 18:45:05 +1100, "Jake Anderson" <[EMAIL PROTECTED]> wrote: >why fly the heater at all? >if the tank is at the right temperature or thereabouts it shouldnt change >that quickly put a sensor in your tank and the heaters in a jacket on the >outside when its hot enough drop the jack

Re: [ERPS] KISS III Propulsion System Test

2002-11-01 Thread Henry Spencer
On Fri, 1 Nov 2002, Jake Anderson wrote: > why fly the heater at all? > if the tank is at the right temperature or thereabouts it shouldnt change > that quickly put a sensor in your tank and the heaters in a jacket on the > outside when its hot enough drop the jacket and hit the button Now you nee

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread forkbomb
Tape heaters are inappropriate for Spike, since the propellant tank is part of the aeroshell and it needs to be very clean aerodynamically in order to get good data. Cole-Palmer sells 316 SS immersion heaters that might be appropriate if we decide we need tank heat. Honestly, I don't think we do

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread Jake Anderson
t; <[EMAIL PROTECTED]> To: "Adrian Tymes" <[EMAIL PROTECTED]> Cc: "ERPS" <[EMAIL PROTECTED]> Sent: Friday, November 01, 2002 6:29 PM Subject: Re: [ERPS] KISS III Propulsion System Test > On Thu, 31 Oct 2002 20:17:48 -0800, Adrian Tymes <[EMAIL PROTECT

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread Randall Clague
On Thu, 31 Oct 2002 20:17:48 -0800, Adrian Tymes <[EMAIL PROTECTED]> wrote: >This makes procedures simpler (fuel whenever, fly whenever after >fuelling), but not the vehicle: it adds another component to what has to >fly. That's correct. It's a tradeoff I'm happy to make. -R -- "...And the las

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread Randall Clague
On Thu, 31 Oct 2002 23:16:31 -0500, "Sean Patrick Daly" <[EMAIL PROTECTED]> wrote: >If in the end, all you are looking to achieve is heating the H2O2 tank up a >bit, I'd go with an even simpler approach by using Nitrous Oxide tank >heaters available at your local performance auto parts shop/catalo

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread forkbomb
On 30 Oct 2002 16:06:50 -0800 "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: > > Seriously, ERPS is interested in developing > technology, and if we just > want to test engines, silver is fine. Catalysts > that work with >90% > peroxide are necessary for operational projects > that soon will need to

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread Adrian Tymes
Randall Clague wrote: On Thu, 31 Oct 2002 18:06:04 -0800, [EMAIL PROTECTED] wrote: A commercial venture that wants to operate year round will need to heat the tanks to keep the peroxide from freezing. Or at least fill the tanks from a larger reservoir, whose temperature is actively mainta

RE: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread Sean Patrick Daly
around the tank. Not too much draw on power and will run on 12/24 volts. Sean -Original Message- From: [EMAIL PROTECTED] [mailto:erps-list-admin@;lists.erps.org]On Behalf Of Randall Clague Sent: Thursday, October 31, 2002 10:41 PM To: ERPS Subject: Re: [ERPS] KISS III Propulsion System Te

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread Randall Clague
On Thu, 31 Oct 2002 18:06:04 -0800, [EMAIL PROTECTED] wrote: >> A commercial venture that wants to operate year round will need to >> heat the tanks to keep the peroxide from freezing. > >Or at least fill the tanks from a larger reservoir, whose temperature is >actively maintained, soon enoug

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread cpwinter
On 29 Oct 2002, at 2:35, Randall Clague wrote: > On 28 Oct 2002 21:34:28 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> > wrote: > > >Because silver melts above 85-90%, electrical heating significantly > >increases the range of catalysts available to us, and because we're > >eventually going to need

Re: [ERPS] KISS III Propulsion System Test

2002-10-31 Thread ShadowMem
And before anyone asks, we will *not* discuss any peroxide enrichment techniques. Dan In a message dated 10/30/2 11:07:17 PM, [EMAIL PROTECTED] writes: << Our purification process currently yields 99% H2O2 by concentration with <1 ppm total dissolved solids. This is from various concentrations r

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread David Masten
On Wed, 2002-10-30 at 21:27, Randall Clague wrote: > On Wed, 30 Oct 2002 18:29:42 -0600, John Carmack > <[EMAIL PROTECTED]> wrote: > > >As I understand it, every single concentration process performs > >incrementally, so you just stop concentrating when you are at the level you > >want... > > T

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Randall Clague
On Wed, 30 Oct 2002 18:29:42 -0600, John Carmack <[EMAIL PROTECTED]> wrote: >As I understand it, every single concentration process performs >incrementally, so you just stop concentrating when you are at the level you >want... The fractional freezing is working fairly well - kudos to all involv

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Randall Clague
On 30 Oct 2002 16:09:55 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: >I'd like to have a higher performance propellant available for Spike, >and I'm sure it wouldn't hurt POGO either. If and when we're >manufacturing peroxide, it'll be at higher concentrations than we can >use, so we'll have

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Adrian Tymes
Sean R. Lynch wrote: On Wed, 2002-10-30 at 16:29, John Carmack wrote: As I understand it, every single concentration process performs incrementally, so you just stop concentrating when you are at the level you want... Tell that to our freezer. The freezer hasn't been producing 99+% peroxid

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Sean R. Lynch
On Wed, 2002-10-30 at 16:29, John Carmack wrote: > As I understand it, every single concentration process performs > incrementally, so you just stop concentrating when you are at the level you > want... Tell that to our freezer. signature.asc Description: This is a digitally signed message p

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread John Carmack
Seriously, ERPS is interested in developing technology, and if we just want to test engines, silver is fine. Catalysts that work with >90% peroxide are necessary for operational projects that soon will need to be able to deal with low temperature launches. Eh? All "operational projects" that

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread John Carmack
At 04:09 PM 10/30/2002 -0800, you wrote: On Tue, 2002-10-29 at 21:33, Randall Clague wrote: > I've read your e-mails. I think you're looking to solve a problem > that is having no effect on our operations, and is therefore not > relevant on the time scale at which we operate. ERPS has historical

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Sean R. Lynch
On Tue, 2002-10-29 at 21:33, Randall Clague wrote: > I've read your e-mails. I think you're looking to solve a problem > that is having no effect on our operations, and is therefore not > relevant on the time scale at which we operate. ERPS has historical > experience chasing solutions to problem

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Sean R. Lynch
On Wed, 2002-10-30 at 09:30, Andrew Case wrote: > My sense is > that the best approach is to preheat the catalyst by firing on a warm > day :-) Simple is good. "I'm sorry, Billy, but winter came early this year, so you're going to have to wait until next year to fly to the moon." Oh wait, Billy w

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Andrew Case
On Wed, 30 Oct 2002, Alex Fraser wrote: > In the light of the thread " more thoughts on catalysts" and on rereading > this post below it occurred to me that there are two iron oxides commonly called > red and black. The formation of steel from iron alloy seems to assure that it > produces red

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Alex Fraser
mixing before engine firing became a pain in the ass, and I found it > impossible to get a even reaction. > > Sean > > -Original Message- > From: [EMAIL PROTECTED] > [mailto:erps-list-admin@;lists.erps.org]On Behalf Of Michael Free > Sent: Wednesday, October 30, 2002 6:

RE: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Sean Patrick Daly
--Original Message- From: [EMAIL PROTECTED] [mailto:erps-list-admin@;lists.erps.org]On Behalf Of Michael Free Sent: Wednesday, October 30, 2002 6:47 AM To: Sean R. Lynch; ERPS; Pierce Nichols Subject: Re: [ERPS] KISS III Propulsion System Test If iron oxide is a good enough catalyst for an o

Re: [ERPS] KISS III Propulsion System Test

2002-10-30 Thread Michael Free
- Original Message - From: "Pierce Nichols" <[EMAIL PROTECTED]> To: "Sean R. Lynch" <[EMAIL PROTECTED]>; "ERPS" <[EMAIL PROTECTED]> Sent: Tuesday, October 29, 2002 12:54 AM Subject: Re: [ERPS] KISS III Propulsion System Test > At 09:3

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 04:26 AM 10/30/2002 +, Ian Woollard wrote: Doesn't iron (oxide) work at high temperature? Preheating might give you a long lived and cheap catalyst. You don't want it self warming though- I think it tends to hard start. Probably depends on the initial oxidization state of the ir

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread John Carmack
At 08:36 PM 10/29/2002 -0800, you wrote: At 08:11 PM 10/29/2002 -0800, Donald Qualls wrote: Say, has anyone tested copper or bronze as a high temperature catalyst? Melting point significantly higher than silver, 1083 C for pure copper; bronzes can be had with either higher or lower melting

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Randall Clague
On 29 Oct 2002 18:08:23 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: >> >Note that I was talking about electrically heating the *catalyst*, not >> >the peroxide. When our reaction starts out milky and then goes clear, >> >it's not the peroxide that's heating up, it's the catalyst. >> >> Is t

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 08:11 PM 10/29/2002 -0800, Donald Qualls wrote: Say, has anyone tested copper or bronze as a high temperature catalyst? Melting point significantly higher than silver, 1083 C for pure copper; bronzes can be had with either higher or lower melting points. The high corrosion resistance of t

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Ian Woollard
Doesn't iron (oxide) work at high temperature? Preheating might give you a long lived and cheap catalyst. You don't want it self warming though- I think it tends to hard start. Donald Qualls wrote: Randall Clague wrote: On 29 Oct 2002 13:55:07 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote:

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Donald Qualls
Randall Clague wrote: On 29 Oct 2002 13:55:07 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: > Unless I'm mistaken, Gizmocopter's battery packs would heat 1kg of tungsten by >3600K. For how long? I don't know that it really matters, as long as it can stay hot until you're up to full flo

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 06:06 PM 10/29/2002 -0800, Sean R. Lynch wrote: You have merely restated your claim rather than saying on what basis you make it. Generally when someone asks you to provide a basis for your claim, you should provide some evidence to back it up. Go read chapter 16 of Pauling's 'Gener

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Tue, 2002-10-29 at 16:12, Randall Clague wrote: > On 29 Oct 2002 13:32:52 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> > wrote: > > >Note that I was talking about electrically heating the *catalyst*, not > >the peroxide. When our reaction starts out milky and then goes clear, > >it's not the pero

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Tue, 2002-10-29 at 16:51, Pierce Nichols wrote: > At 01:25 PM 10/29/2002 -0800, Sean R. Lynch wrote: > >On Tue, 2002-10-29 at 08:09, Pierce Nichols wrote: > > > Any catalyst with substantial activity at elevated temperature > > > will be noticeably incompatible at room temperature. > >

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 01:25 PM 10/29/2002 -0800, Sean R. Lynch wrote: On Tue, 2002-10-29 at 08:09, Pierce Nichols wrote: > Any catalyst with substantial activity at elevated temperature > will be noticeably incompatible at room temperature. On what basis do you make this claim? Platinum is almost completel

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Randall Clague
On 29 Oct 2002 13:32:52 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: >Note that I was talking about electrically heating the *catalyst*, not >the peroxide. When our reaction starts out milky and then goes clear, >it's not the peroxide that's heating up, it's the catalyst. Is that all you're

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Randall Clague
On 29 Oct 2002 13:55:07 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: >You mean we haven't seen catalyst temperature problems since we started >using *silver* which will be useless when we go to higher strength >peroxide. This makes silver a "low temperature catalyst" in my mind. It >works in

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Tue, 2002-10-29 at 02:35, Randall Clague wrote: > I'm not enthused about electrically heated catalysts, because they are > not as simple as ambient temperature catalysts, and we have not seen > catalyst temperature problems since before we starting getting good > data a couple years ago. There

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread David Weinshenker
"Sean R. Lynch" wrote: > Note that I was talking about electrically heating the *catalyst*, not > the peroxide. When our reaction starts out milky and then goes clear, > it's not the peroxide that's heating up, it's the catalyst. I've suggested that a "multi-stage" pack could be made: we observed

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Tue, 2002-10-29 at 02:35, Randall Clague wrote: > A commercial venture that wants to operate year round will need to > heat the tanks to keep the peroxide from freezing. Heating the > peroxide as a performance enhancement strikes me as unwise. It may be > necessary in the future - we don't kno

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Tue, 2002-10-29 at 08:09, Pierce Nichols wrote: > Any catalyst with substantial activity at elevated temperature > will be noticeably incompatible at room temperature. On what basis do you make this claim? Platinum is almost completely uncatalytic to peroxide at room temperature. I ca

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Henry Spencer
On Tue, 29 Oct 2002, Pierce Nichols wrote: > > Beryllium melts at 1278C, but it's not a transition > >metal. > > It's also toxic as all get out. That is a bad property. It's also brittle, and hence very difficult to work with. > ...Also, the oxide layer > on Al forms on contact with a

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Alex Fraser
My reasoning for warming the H2O2 was to lesson the energy needed to boil off the 15% water in it. With the danger of instability removed (just pretend) if you heated the mix to 102C (or whatever the boiling point of water is at your tank pressure) then it would flash to steam as you squirt it

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 12:59 AM 10/29/2002 -0800, Sean R. Lynch wrote: Silver melts at 961.93C. Aluminum melts at 660.37C, so it's clearly out. Nickel melts at 1453C, so it's a definite candidate assuming it will form an oxide and the oxide is catalytic at temperatures we can reasonably heat it to electrically.

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Andrew Case
On Mon, 28 Oct 2002, Pierce Nichols wrote: > The actual working catalyst should be a ceramic composed of the > best catalysts found in the search. Alternatively, you could try looking at the available commercial ceramics and pick a few with high proportions of possibly interesting oxides in them

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Randall Clague
On Mon, 28 Oct 2002 23:20:28 -0500, Alex Fraser <[EMAIL PROTECTED]> wrote: >Is there actual test data on this temperature performance relationship? Yes, in the 1960 Bepco-FMC paper. They measured the temperature of the peroxide, not that of the catalyst, but they saw a significant effect. Activ

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Randall Clague
On 29 Oct 2002 00:59:31 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: >Nichrome wire anyone? We could make a catpack out of used model rocket >ignitors :) If I was going to test an electrically heated catalyst, I would start with nichrome. Keep It Simple. I'm not enthused about electricall

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Randall Clague
On Tue, 29 Oct 2002 00:38:54 -0800, Pierce Nichols <[EMAIL PROTECTED]> wrote: > Nickel is one of the few transition metals that does *not* have a >bad relationship with peroxide. I consider the most interesting targets of >investigation to be Pt, Pd, Rh, Re, Co, & Ir, mostly due to the c

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Randall Clague
On 28 Oct 2002 21:34:28 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: >Because silver melts above 85-90%, electrical heating significantly >increases the range of catalysts available to us, and because we're >eventually going to need to deal with the problem A commercial venture that wants to

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread David Masten
On Tue, 2002-10-29 at 00:59, Sean R. Lynch wrote: > Is it aluminum oxide that we're making inside our tanks when we > passivate them? Clearly both of these are pretty compatible with > peroxide at reasonable temperatures, but heat them up and who knows? > Aluminum forms an oxide layer immediately

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Tue, 2002-10-29 at 00:23, Sean R. Lynch wrote: > What if, in general, it's *only* the oxides of these metals that are > catalytic and not the metals themselves at all? What if silver is only > so good because its oxide is so tenacious? If this is the case, then the > process would be clear: fin

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 12:23 AM 10/29/2002 -0800, Sean R. Lynch wrote: On Mon, 2002-10-28 at 21:54, Pierce Nichols wrote: > All of the catalysts for peroxide that I have heard > tested or floated in any way are transition metals or their oxides. > Anecdotal evidences (such as the requirement for 'burning in' a silver

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Mon, 2002-10-28 at 21:54, Pierce Nichols wrote: > All of the catalysts for peroxide that I have heard > tested or floated in any way are transition metals or their oxides. > Anecdotal evidences (such as the requirement for 'burning in' a silver > pack) indicates that it's the oxides that have

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 12:06 AM 10/29/2002 -0800, Sean R. Lynch wrote: On Tue, 2002-10-29 at 00:05, Pierce Nichols wrote: > See my original idea, and delete the idea of making a compound > catalyst. Catalogue oxide/base metal pairs with attractive properties, make > samples, and test them. Sounds good to

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Tue, 2002-10-29 at 00:05, Pierce Nichols wrote: > See my original idea, and delete the idea of making a compound > catalyst. Catalogue oxide/base metal pairs with attractive properties, make > samples, and test them. Sounds good to me, as long as you still mean to preheat them. Even

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Pierce Nichols
At 11:58 PM 10/28/2002 -0800, Sean R. Lynch wrote: On Mon, 2002-10-28 at 22:12, Pierce Nichols wrote: > At 10:19 PM 10/28/2002 -0800, David Weinshenker wrote: > >Pierce Nichols wrote: > > > The actual working catalyst should be a ceramic > > > composed of the best catalysts found in the search. >

Re: [ERPS] KISS III Propulsion System Test

2002-10-29 Thread Sean R. Lynch
On Mon, 2002-10-28 at 22:12, Pierce Nichols wrote: > At 10:19 PM 10/28/2002 -0800, David Weinshenker wrote: > >Pierce Nichols wrote: > > > The actual working catalyst should be a ceramic > > > composed of the best catalysts found in the search. > > > >Pressed into pellets and fired at high temperat

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Pierce Nichols
At 10:19 PM 10/28/2002 -0800, David Weinshenker wrote: Pierce Nichols wrote: > The actual working catalyst should be a ceramic > composed of the best catalysts found in the search. Pressed into pellets and fired at high temperature, no doubt... :) Something like that :P. -p

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread David Weinshenker
Pierce Nichols wrote: > The actual working catalyst should be a ceramic > composed of the best catalysts found in the search. Pressed into pellets and fired at high temperature, no doubt... :) -dave w ___ ERPS-list mailing list [EMAIL PROTECTED] http://

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Pierce Nichols
At 09:34 PM 10/28/2002 -0800, Sean R. Lynch wrote: For example, according to Dan's tests platinum only works well at high temperatures. I was hoping we could use something a little less expensive, though. Stainless steel maybe? :) Iron oxide is a catalyst. Stainless steel doesn't for

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Sean R. Lynch
On Mon, 2002-10-28 at 16:49, Randall Clague wrote: > Why? Armadillo is having performance problem which they suspect are > due to cold. ERPS isn't. Because silver melts above 85-90%, electrical heating significantly increases the range of catalysts available to us, and because we're eventually

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread ShadowMem
There is a little bit of theoretical performance increase at higher temperatures, *but*, the peroxide also gets less dense, which would require slightly bigger tanks. Either effect is probably in the noise of what we could measure. This assumes of course, that its warm enough to fully catalyze.

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Alex Fraser
Is there actual test data on this temperature performance relationship? If you get 430 lbf. at 74 F would it be worth it to heat to 110 F. ? What is the danger point for heating 85% H2O2? Randall Clague wrote: > On 28 Oct 2002 15:32:36 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> > wrote: > > >> >

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Henry Spencer
> ...Would tungsten work or would that have to be too hot? In addition to the oxidation problems already noted, tungsten has a bad habit of being brittle at room temperature. Henry Spencer

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Randall Clague
On 28 Oct 2002 15:32:36 -0800, "Sean R. Lynch" <[EMAIL PROTECTED]> wrote: >> >Did you guys read the Armadillo update, in particular the part about >> >suspected correlation between milky exhaust and initial temperature of >> >peroxide. >> >> Yep. Initial peroxide temperature has a pronounced

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread ShadowMem
IIRC, its not an adherent, tenacious oxide, like what forms on stainless steels and other high temp alloys. This would allow the entire volume of W to oxidize, yielding dust in the exhaust. Aside from this, I don't know how good a catalyst W or its oxide is. Dan In a message dated 10/28/02 3:51

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Sean R. Lynch
On Mon, 2002-10-28 at 15:43, [EMAIL PROTECTED] wrote: > Tungsten easily oxidizes at high temps. Is tungsten oxide a good catalyst or does it end up going away in your exhaust? -- Sean R. Lynch KG6CVV http://www.chaosring.org/~seanl/ signature.asc Description: This is a digitally signed messa

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread ShadowMem
Tungsten easily oxidizes at high temps. Dan In a message dated 10/28/02 3:33:18 PM, [EMAIL PROTECTED] writes: << Would tungsten work or would that have to be too hot? >> ___ ERPS-list mailing list [EMAIL PROTECTED] http://lists.erps.org/mailman/listi

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Sean R. Lynch
On Mon, 2002-10-28 at 15:19, Randall Clague wrote: > On Mon, 28 Oct 2002 15:12:23 -0500, Alex Fraser <[EMAIL PROTECTED]> > wrote: > > >Did you guys read the Armadillo update, in particular the part about > >suspected correlation between milky exhaust and initial temperature of > >peroxide. >

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Randall Clague
On Mon, 28 Oct 2002 15:12:23 -0500, Alex Fraser <[EMAIL PROTECTED]> wrote: >Did you guys read the Armadillo update, in particular the part about >suspected correlation between milky exhaust and initial temperature of >peroxide. Yep. Initial peroxide temperature has a pronounced effect on cat

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Alex Fraser
Did you guys read the Armadillo update, in particular the part about suspected correlation between milky exhaust and initial temperature of peroxide. On the static test (KISS III) did you make a note of the initial temperature? I'm not sure of the local conditions where you plan to fly, but I t

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread ShadowMem
Also, KISS III when fully loaded with 'fuel', 10 liters of peroxide, plus the extra plumbing/pressurant tank weight, will weigh about 30 more pounds at liftoff compared to KISS II. The gross liftoff weight (GLOW) of KISS II was about 51 pounds, and KISS III will be about 80 pounds. Thus, we want

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Michael Wallis
Alex Fraser wrote: > Good News > > Please outline the goals for the KISS III flight. The KISS III vehicle (KISS three not one hundred and eleven), is a follow-on to the successful KISS II campaign to fly a simple ballistic path with an ERPS designed and built vehicle powered by an ERPS desi

Re: [ERPS] KISS III Propulsion System Test

2002-10-28 Thread Alex Fraser
Good News Please outline the goals for the KISS III flight. David Masten wrote: > We tested the KISS III constant pressure propulsion section today.The > test was far from ideal, but we verified what we needed. > > The data acquisition unit just refused to work, a DATAQ that we bought > just

[ERPS] KISS III Propulsion System Test

2002-10-27 Thread David Masten
We tested the KISS III constant pressure propulsion section today.The test was far from ideal, but we verified what we needed. The data acquisition unit just refused to work, a DATAQ that we bought just for testing the KISS engine. I have the new data acquisition hardware on hand, but it was not