sferrin said:exactly what was NASP's propulsion system to take it from 0 to Mach 7 suppose to be? ???
shockonlip said:Pretty Interesting!
shockonlip said:Yes Dan, definitely loud.
You're right, an ejector.
I think we're going to hear more about cryo-cooling however.
You can get a nice pressure ratio!
Meteorit said:Does anyone have a three-view drawing of the "duPont Government Baseline" vehicle? Also any dimensional info besides the TOGW of 50,000 pounds? I've been thinking for some time of making a 3D model of this design to go along my 3D Tu-2000A that shares a very similar configuration. Would make for an interesting comparison; also perhaps eventually have it flyable in the Orbiter simulator.
Image from The Hypersonic Revolution. Case Studies in the History of Hypersonic Technology. Vol.3 referenced above.
Meteorit said:For those who thought Star Wars was too realistic: duPont baseline first deploys a satellite from a sizeable payload bay and then takes some passengers to a space station.
Also has a lovely NASP scale model (I want one! ;D).
I bought several X-30 concepts from a Pratt & Whitney engineer and this is a duplicate. As a part of a five-company team, Pratt & Whitney pursued propulsion technologies for the National Aerospace Plane (NASP); the prototype aircraft was designated X-30. This model was made sometime in the 1980’s by Penwal, one of the companies founded by Topping Models alumni (Walt Hyatt with Jerry Pennington) after Topping’s closing in 1965. It is in excellent shape, with the tiniest bit of yellowing that should clean up nicely with Novus #2 cleaner/polish (although I would just leave it). But there are no chips, breaks, dings, scrapes, flakes, or any other flaws anywhere. Never broken, never repaired--it’s in excellent condition. The fuselage is just over 16” long and the wingspan is 4 inches. The model is made of a solid, heavy and hard injection-molded material and is exceptionally well finished. There are red and blue markings running the length of the fuselage and up the vertical stabilizer. The cockpit windows are gray, the nose is black. Small American flags mark the left wing and each side of the stabilizer. The words “United States of America” run along both sides of the fuselage. The model sits firmly on the stand via two deep pins but is easily removed. The like-new base is a richly finished custom wood faceted triangle with black Plexiglas upright. There is a small Pratt & Whitney eagle logo on it, and a gold nameplate with “X-30 National Aerospace Plane” printed in black. Underneath is a mint label bearing Penwal’s name, logo, and Chino address.The three original protective felt dots are like new. Model will be fastidiously packed with insurance and tracking included.
Mark Nankivil said:Thanks Triton! Mark
Gotta admire that heatproof strobelight on the X-30's bottom.
DSE said:Some additional NASP art:
flateric said:DSE, thanks for these rarities
Six Copper Canyon/NASP tunnel entries were completed in the 16’TT between 1984 and 1993. Hypersonic technology development in the 16’TT actually started prior to the NASP program with an air breathing launch vehicle study in 1974 and continued up to facility shutdown in 2004 with nine Pegasus/X-43 entries.
The photograph shows a front view of one of the early Copper Canyon NASP configurations mounted in the 16-Foot Transonic Tunnel. The configuration was a winged cone (forebody/truncated cone (afterbody) with a ring of air-breathing supersonic combustion ramjets (or scramjets) completely circling the body.
flateric said:Six Copper Canyon/NASP tunnel entries were completed in the 16’TT between 1984 and 1993. Hypersonic technology development in the 16’TT actually started prior to the NASP program with an air breathing launch vehicle study in 1974 and continued up to facility shutdown in 2004 with nine Pegasus/X-43 entries.
DSE said:Hmmm, not sure why they stopped with the history at that point. The final test was also related to hypersonic airbreathing propulsion. The NASP 5B powered model was retested to get vehicle nozzle data to verify the methods being to predict the aftbody performance for the ISTAR vehicle in the transonic regime. Predicting where the overexpanded engine flow shocks back up to ambient is a tough problem especially when doing less than full up hi-res 3-D CFD during configuration development studies. In some cases the simpler methods didn't even get the sense of the pitching moment correct.
flateric said:I just wonder how funny Boeing's 'Conical Accelerator' NASP configuration would look resting on its - quite trickily designed I assume - landing gears.
quellish said:The original du Pont design had no landing gear:
"To save weight, duPont’s concept had no landing gear. It lacked reserves of fuel; it was to reach orbit by burning its last drops. Once there it could not execute a controlled deorbit, for it lacked maneuvering rockets as well as fuel and oxidizer for them. DuPont also made no provision for a reserve of weight to accommodate normal increases during development."
flateric said:I just wonder how funny Boeing's 'Conical Accelerator' NASP configuration would look resting on its - quite trickily designed I assume - landing gears.
Delta Clipper was a honest Heinlein-style VTVL rrrocket from my childhood books, and bad things happen to her when she tried to laid in its back (the thing what Conical Accelerator NASP should have done repeatedly in standart mode)DSE said:How much different would this had been than DC-X?
flateric said:nope
that one in Langley WT
other clues are
http://www.secretprojects.co.uk/forum/index.php/topic,250.msg44404.html#msg44404
http://www.secretprojects.co.uk/forum/index.php/topic,5238.msg41501.html#msg41501
http://www.secretprojects.co.uk/forum/index.php/topic,250.msg2636.html#msg2636
According to Hypersonic Revolution Vol.III by Larry Schweikart -
Two Boeing design studies were completed, one was 'winged body', so-called government baseline, i.e. scaled-up duPont design, so basically all published illustrations if refered to this study is not far away from truth.
Later Boenig shifted to Langley-promoted (sic!) conical accelerator, but entered a serious problems as result was VERY long vehicle with myriad stability/engine control problems. Boeing was downselected from competition.