Return-Path: Received: from [67.20.112.52] (account rob HELO Logan.com) by logan.com (CommuniGate Pro SMTP 4.2b5) with ESMTP-TLS id 145178 for lml@lancair.net; Tue, 08 Jun 2004 23:32:40 -0400 Message-ID: <40C684D6.1070702@Logan.com> Date: Tue, 08 Jun 2004 23:32:38 -0400 From: Rob Logan User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.6) Gecko/20040113 X-Accept-Language: en-us, en MIME-Version: 1.0 To: lml@lancair.net Subject: Rutan tries for 100-km. suborbital flight with SpaceShipOne Content-Type: multipart/mixed; boundary="------------040604070301060401000206" This is a multi-part message in MIME format. --------------040604070301060401000206 Content-Type: text/plain; charset=us-ascii; format=flowed Content-Transfer-Encoding: 7bit Taken without permission from Aviation Week & Space Technology June 7 2004 -Rob Rutan tries for 100-km. suborbital flight with SpaceShipOne Scaled Composites is opening its first attempt at a 100-km. (328,000-ft.) suborbital flight, inviting the public to view the June 21 event from its Mojave, Calif., airport home base, from which the SpaceShipOne craft will take off and land, and the rocket boost will be visible. Company founder Burt Rutan hopes a successful flight will accelerate broader developments in space tourism. The plan is to next shoot for the tourism-promoting Ansari X Prize by reaching 100km. with the added weight equivalent of two passengers, and repeat the flight within two weeks. The rocket glider reached 211,400 ft. on May 13 with a 55-sec. firing of its hybrid solid rocket engine. Scaled expects to reach the 328,000-ft. design altitude with a full-duration 80-sec. burn just two weeks from now. The main novelties of the next flight are the longer burn, an untried larger rocket nozzle, higher temperatures and Mach numbers, and low dynamic pressure at burnout. The last two flights carried a full load of hydroxyl-terminated polybutadiene rubber fuel in the rocket case and nitrous oxide oxidizer in the tank behind the cockpit, and were at nearly maximum gross weight. The rocket was shut off in mid-burn by stopping the oxidizer flow, but the next flight will fully expend it. SAFETY OF THE LONGER BURN was tested on the ground by taking a rocket case that had gone through a full-duration run and firing it again with a 100-sec. flow of nitrous oxide. This burned the remnants of fuel, consumed the silica phenolic heat-resistant liner, and started to smoke the carbon fiber/epoxy outer case, but did not penetrate it. The larger nozzle has a higher expansion ratio that will yield more thrust and efficiency at high altitude. It has not been tested on the ground because it overexpands the exhaust there, leading to flow separation and turbulence within the nozzle. Tests of the short nozzle show that as the case structure around it warms up, the nozzle moves a little bit, and motion sensors are part of the automatic shutdown safety system. The last flight reached Mach 2.5 during boost and heating was recorded with temperatures a little less than expected. The red thermal proctection coating on the leading edges, nose and belly of SpaceShipOne was not damaged and remains in place for the June 21 flight, which is expected to reach about Mach 3.5. However, peak equivalent airspeed will not be any higher because the high Mach number will be achieved at the edge of the atmosphere, where the equivalent airspeed is low. The extra heat of higher Mach will damage the thin coating, which can be replaced. Control effectiveness was good on the last flight but roll-yaw coupling made it difficult to fly. It achieved a super-sonic entry for the first time, reach Mach 1.9 while in the "feather" configuration, which pops up the aft wing and tail booms to enter at a high-drag 53-65-deg. body angle of attack. There were roll oscillations in feather but they were slow enough that pilot Mike Melvill was able to manually damp them. There is no fly-by-wire on SpaceShipOne. The oscillations might be due to remaining liquid oxidizer sloshing in the tank, but the tank will be emptied on the 100-km. flight. The main control concern for the record flight is that the end of the longer burn is occurring at the fringes of the atmosphere and control authority to counter thrust asymmetries from nozzle erosion will be weak because of the low equivalent airspeed. Add to this whatever changes in control effectiveness there are with the higher Mach number. The computational fluid dynamics says it is OK but the pilot will be earning his salary. Attitude is controlled with cold gas jets during the upward coast through vacuum, but they are very weak compared to a conventional surface biting into thick air. The May 13 flight was a big jump in envelope expansion by going to Mach 1.9 from Mach 0.88 in feather configuration, as well as jumping to Mach 2.5 from Mach 1.6 during the boost. THE INSTRUMENT DISPLAY FAILED on that flight about one-third of the way into the burn, but Melvill continued the trajectory by referencing the horizon through the windows and was able to reach the target apogee. The problem is believed to be the potentiometer that adjusts display brightness - the calculations proceeded correctly but the acceleration pulled the wiper off the contact. Once the motor stopped, the display came back on. The pot has since been hard-wired. The public flight to 100 km. is in contrast to prior tests, which have been a private development program though brief flight test notes have been posted on the web. "It's a legitimate 100-km. spaceflight, done for the first time by a private firm instead of the government, with a civilian as the commander," Rutan said. 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