Return-path: X-Andrew-Authenticated-as: 7997;andrew.cmu.edu;Ted Anderson Received: from holmes.andrew.cmu.edu via trymail for +dist+/afs/andrew.cmu.edu/usr1/ota/space/space.dl@andrew.cmu.edu (->+dist+/afs/andrew.cmu.edu/usr1/ota/space/space.dl) (->ota+space.digests) ID ; Wed, 12 Apr 89 05:16:45 -0400 (EDT) Message-ID: Reply-To: space+@Andrew.CMU.EDU From: space-request+@Andrew.CMU.EDU To: space+@Andrew.CMU.EDU Date: Wed, 12 Apr 89 05:16:37 -0400 (EDT) Subject: SPACE Digest V9 #361 SPACE Digest Volume 9 : Issue 361 Today's Topics: Re: Soviet Mars probes - ZOND 2. Re: Success with cold fusion reported Re: more on Liberty Bell 7 (and other s'craft) Power vs Energy Possible Life on Venus: A Question Re: Possible Life on Venus: A Question Questions and Henry Eggs in space (was NSS Hotline Update 3/31/89) Re: Asteroids and Pd fusion Re: Room Temperature fusion - possible indications? Re: space news from Feb 13 AW&ST Re: Asteroids and Pd fusion ---------------------------------------------------------------------- Date: 10 Apr 89 18:42:01 GMT From: prism!ccoprmd@gatech.edu (Matthew DeLuca) Subject: Re: Soviet Mars probes - ZOND 2. In article <8904101356.AA02908@decwrl.dec.com> klaes@mtwain.dec.com (CUP/ML, MLO5-2/G1 8A, 223-3283) writes: > > In regards to Steve Roseman's reply about the 1964 Soviet Mars >probe ZOND 2... I always thought that the Zond series was a potential lunar capsule, to compete with Apollo, and when Apollo 11 landed, the series was allowed to 'die'. What's the real story? -- --------------------------------------------------------------------------------Matthew DeLuca : Georgia Institute of Technology : Certainty is the lot of those who ARPA: ccoprmd@hydra.gatech.edu : do not question. -------------------------------------------------------------------------------- ------------------------------ Date: 10 Apr 89 06:50:52 GMT From: ucsdhub!sdsu!frost@sdcsvax.ucsd.edu (Richard Frost) Subject: Re: Success with cold fusion reported In article <16627@electron.mips.COM>, jimiii@mips.COM (Jim Warford) writes: > In article <3634@sdsu.UUCP> frost@sdsu.UUCP (Richard Frost) writes: > > > >Although utility companies are required to by any excess power you generate > >YOU are responsible for purchasing a synchonous interface to the grid ( a > >synchronous inverter if you're generating DC) plus a new meter and pay for > >periodic calibration inspections by the utility company. > > > I believe you also have to provide 1 million dollars in liability insurance > just in case your equipment malfunctions and wreaks havoc on the electric > companies equipment. > --jimiii@mips.com In my experience with such projects, no liability insurance was required by the homeowner. Such sites were in rural areas of Northern California (San Francisco is in the middle of the state!!) -------- and the electric power being generated was only a few kilowatts. On a different note, several folks have mentioned that cheap fusion powered generators won't affect auto's too much. Think again. Electric autos are becoming a reality -- witness the Solar Max. Not that I would recommend a solar or a fusion source IN a commuter car. How about we just charge 'em off the grid, or at home? However, I agree that the overhead to convert your auto or for GM to tool up for electric autos is staggering. But really people, we need to slow down our exhaust emmisions while we've still got a healthy atmosphere. sdsu!frost@ucsd.edu ------------------------------ Date: 11 Apr 89 00:09:34 GMT From: ames.arc.nasa.gov!mike@ames.arc.nasa.gov (Mike Smithwick) Subject: Re: more on Liberty Bell 7 (and other s'craft) In article <1726@wpi.wpi.edu> tmurphy@wpi.wpi.edu (Tom [Chris] Murphy) writes: mmm@cup.portal.com (Mark Robert Thorson) writes: <>A few years ago, someone mentioned some Apollo hardware was in the ocean <>(I think it was the LEM from Apollo-13). < jd3l+@andrew.cmu.edu (Jean-Marc Debaud) writes: >There is a question that has been distrubing me lately, > >We discover not a long ago living "parasites" that are >very close to paramecia organism very deep in the >Atlantique Ocean. What is surprising is the capacity of >those organism to live and reproduce in very hot water >located near permanent volcanic activities. Are you sure that these organisms are similar to paramecia? I have heard of archaebacteria living in very hot water, but no eukaryotes. At any rate, if they are free-living, they are not parasites. >According to common knowledge (I am a logician not >a biologist) I thougth that proteins as well as DNA chains >could not be replicated and therefore not formed under high >temperature. Certain proteins are stable at quite high temperatures (80`C is not uncommon), and using various measures an organism can stabilize its proteins and DNA. Such measures include maintaining very high internal salt concentrations and other means of ensuring that the ratio of water to everything else is small (but nonzero). >Furthermore, my understanding was that the reasons above >(temperature, pressure) were the motive why scientist could >not beleive of forms of life on Venus. So do we have to scrap >this belief and restart again ? > >Or am I missing anything here ? One requirement of terrestrial life is that the water within it be liquid, whatever the temperature and pressure. Things have been found that can grow at 135`C, and certain archaebacteria have successfully been cultured in the laboratory at 112`C. However, all of these organisms must be kept under enough pressure to keep them from boiling when they are grown at those temperatures. Such pressures are found at the bottom of our oceans. However, at temperatures over the critical point of water, such as those found on Venus, no amount of pressure will keep the water liquid. Therefore, life with a terrestrial biochemistry will not be able to exist on Venus. Of course, this does not rule out some form of life with a totally different kind of biochemistry. -- | Lucius Chiaraviglio | ARPA: chiaravi@silver.bacs.indiana.edu BITNET: chiaravi@IUBACS.BITNET (IUBACS hoses From: fields; INCLUDE RET ADDR) ARPA-gatewayed BITNET: chiaravi%IUBACS.BITNET@vm.cc.purdue.edu Alt ARPA-gatewayed BITNET: chiaravi%IUBACS.BITNET@cunyvm.cuny.edu ------------------------------ Date: 10 Apr 89 18:41:55 GMT From: rochester!rocksanne!bozo!kirby@cu-arpa.cs.cornell.edu (Mike Kirby (co-op)) Subject: Questions and Henry Two Questions: 1) Henry, do you have anything positive to say about the U.S. space program? I mean do we do anything right anymore? 2) What is the pegasus? Michael Kirby mpk9172@ritvax.bitnet mpk9172%ritcv@rit.cs.edu ------------------------------ Date: 10 Apr 89 17:15:34 GMT From: ncrlnk!ncrcce!johnson@uunet.uu.net (Wayne D. T. Johnson) Subject: Eggs in space (was NSS Hotline Update 3/31/89) Someone missed a great oportunity: CapCom: Columbia, Houston here, good morning. Columbia: Theres no one here but us chickens, cluck, cluck... -- Wayne Johnson (Voice) 612-638-7665 NCR Comten, Inc. (E-MAIL) W.Johnson@StPaul.NCR.COM or Roseville MN 55113 johnson@c10sd1.StPaul.NCR.COM These opinions (or spelling) do not necessarily reflect those of NCR Comten. ------------------------------ Date: 10 Apr 89 21:10:17 GMT From: pacbell!pbhya!whh@ames.arc.nasa.gov (Wilson Heydt) Subject: Re: Asteroids and Pd fusion In article <1989Apr8.212905.131@utzoo.uucp>, henry@utzoo.uucp (Henry Spencer) writes: > In article <10346@nsc.nsc.com> andrew@nsc.nsc.com (andrew) writes: > >... The existence of a heatsink at 3 degK should be a great help for > >the engine design... > > Not as much as you think. Getting the heat out to that heatsink is > *not* a trivial problem. The shuttle uses the entire inner surface of > its payload-bay doors as a heat radiator. If you look at pictures of > the space station, you'll see two sets of big flat panels sticking > out -- solar panels, and radiators. Fusion rockets are likely to have > quite serious cooling problems, at least in high-performance versions. > (Chemical rockets dump heat into their fuel, but a high-performance > fusion rocket doesn't use fuel quickly enough for that approach to work.) As I recall--and I'm sure I'll get some fairly hot replies if I'm wrong-- that the rate of radiation of energy varies as the 4th power of the absolute temperature. Since the Shuttle is working a rather low temperatures, it's no surprise that it needs a large surface. It is also short on total energy supplies. For a fusion rocket, why not use a small, very hot, radiator to take advantage of increased radiator effectiveness? (This *ought* to work for the Shuttle, too, and I don't know why it wasn't done. Possibly because of limitations in working fluids?) --Hal ========================================================================= Hal Heydt | In the old days, we had wooden Analyst, Pacific*Bell | ships sailed by iron men. Now 415-645-7708 | we have steel ships and block- whh@pbhya.PacBell.COM | heads running them. --Capt. D. Seymour ------------------------------ Date: Mon, 10 Apr 1989 11:17-EDT From: Dale.Amon@H.GP.CS.CMU.EDU Subject: Re: Room Temperature fusion - possible indications? > And of course, this will play >hell< with those who promote a > return to the Gold Standard! ;^) Only those who are religious about the particular monetary standard. Most gold standard supporters just want money to be a competitive market like anything else. There can be government script, private bank notes, gold, silver, hog bellies, rights to energy output units, whatever. It really doesn't matter so long as the money supply is not in monopolistic hands. And doesn't it seem rather foolish to have the "one and only official" money printed by the same people who have the power to tax and spend? There seems to be a tiny conflict of interest here... ------------------------------ Date: 10 Apr 89 15:19:34 GMT From: thorin!zeta!leech@mcnc.org (Jonathan Leech) Subject: Re: space news from Feb 13 AW&ST In article <1989Apr10.025652.28387@utzoo.uucp> henry@utzoo.uucp (Henry Spencer) writes: >Phobos 2 enters Mars orbit Jan 29. [I'll skip the details, since we >all know that Phobos 2 is now dead. They really should have launched >three of them.] Perhaps the effort would better be spent putting more reliable hardware on board the spacecraft, and better trained personnel on the ground. Of what use would *three* failed Mars probes be? :-) Unrelated topic: anyone interested in sharing a hotel room at the Chicago Space Development Conference? Respond by email, please. -- Jon Leech (leech@cs.unc.edu) __@/ ``God is more interested in your future and your relationships than you are.'' - Billy Graham ------------------------------ Date: 10 Apr 89 21:25:22 GMT From: cbmvax!jesup@uunet.uu.net (Randell Jesup) Subject: Re: Asteroids and Pd fusion In article <1989Apr8.212905.131@utzoo.uucp> henry@utzoo.uucp (Henry Spencer) writes: >In article <10346@nsc.nsc.com> andrew@nsc.nsc.com (andrew) writes: >>... The existence of a heatsink at 3 degK should be a great help for >>the engine design... > >Not as much as you think. Getting the heat out to that heatsink is >*not* a trivial problem. The shuttle uses the entire inner surface of >its payload-bay doors as a heat radiator. If you look at pictures of >the space station, you'll see two sets of big flat panels sticking >out -- solar panels, and radiators. Fusion rockets are likely to have >quite serious cooling problems, at least in high-performance versions. >(Chemical rockets dump heat into their fuel, but a high-performance >fusion rocket doesn't use fuel quickly enough for that approach to work.) There's a bit of confusion here (especially in the original message). First, the fuel (for energy) is deuterium. Second, the fuel (in terms of reaction mass) is fairly arbitrary. Hydrogen isn't bad, but it's pretty light. Mercury (as in ion engines) is nice and heavy, makes for good specific impulse for an electric engine. In addition, given minimal mining ability, mass from the asteroid can be used if need be. Second, while not 3 deg K, the asteroids mass might make a nice, convenient heat sink. Also, its surface makes a nice place to put radiators. Third, so long as you don't care how fast the asteroid get to you, you can use an arbitrarily small amount of palladium for the fusion reactor. Remember, the fuel is the deuterium. So what if it takes a few centuries? :-) The real question is to figure out how many watts can be produced/cc (F&P results may not be indicative of what is possible, especially with D-T or T-T fusion, but they get 26w/cc); and then figure out the efficiency of your heat engine and specific impulse of your fuel, etc; and then figure out how long it takes to produce the delta-v. Of course, I'm no rocket scientist. :-) -- Randell Jesup, Commodore Engineering {uunet|rutgers|allegra}!cbmvax!jesup ------------------------------ End of SPACE Digest V9 #361 *******************