DARPA Hypersonic Vehicle Splash Down Confirmed | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-05.13.24

Airborne-NextGen-05.14.24

Airborne-Unlimited-05.15.24 Airborne-AffordableFlyers-05.16.24

Airborne-Unlimited-05.17.24

Wed, Aug 24, 2011

DARPA Hypersonic Vehicle Splash Down Confirmed

Flight 1 Engineering Changes Believed Effective

During a test flight Thursday, 11 August, DARPA's Falcon HTV-2 scramjet powered aircraft experienced a flight anomaly post perigee and into the vehicle's climb. The anomaly prompted the vehicle's autonomous flight safety system to use the craft's aerodynamic systems to make a controlled descent and splash down into the ocean, according to a DARPA news release. Controlled descent is a term typically associated with a human-in-the-loop directing or guiding the unscheduled landing of an aircraft. For DARPA's Hypersonic Technology Vehicle 2 (HTV-2) controlled descent takes on new meaning thanks to the vehicle's safety system.

"We've confirmed that the HTV-2 made impact with the Pacific Ocean along its flight trajectory as planned in the event of an anomaly," explained Air Force Maj. Chris Schulz, DARPA HTV-2 program manager and PhD in aerospace engineering. "This flight safety system is a significant engineering advance in that the system prompts a vehicle to monitor the parameters under which it is operating and exercise safety protocols completely autonomously should those parameters be breached."

"According to a preliminary review of the data collected prior to the anomaly encountered by the HTV-2 during its second test flight," said DARPA Director Regina Dugan, "HTV-2 demonstrated stable aerodynamically controlled Mach 20 hypersonic flight for approximately three minutes. It appears that the engineering changes put into place following the vehicle's first flight test in April 2010 were effective. We do not yet know the cause of the anomaly for Flight 2."

A detailed analysis conducted by an independent Engineering Review Board following the first flight test, prompted engineers to adjust the vehicle's center of gravity, decrease the angle of attack flown and use the onboard reaction control systems to augment vehicle flaps during the vehicle's second flight test. Those changes appear to have been effective. "An initial assessment indicates," said Schulz, "that the Flight 2 anomaly is unrelated to the Flight 1 anomaly."

FMI: www.darpa.mil

Advertisement

More News

ANN's Daily Aero-Term (05.16.24): Instrument Runway

Instrument Runway A runway equipped with electronic and visual navigation aids for which a precision or nonprecision approach procedure having straight-in landing minimums has been>[...]

ANN's Daily Aero-Linx (05.16.24)

Aero Linx: Alaska Airmen's Association The Alaska Airmen's Association includes over 2,000 members—we are one of the largest General Aviation communities in the country. We s>[...]

Airborne 05.15.24: Ghost Sq MidAir, B-2 Junked, Dream Chaser Readies

Also: Flt School Security, G600 Steep-Approach, Honduran Aid, PW545D Cert Two aircraft performing at the Fort Lauderdale Air Show clipped wings during a routine last Sunday, spooki>[...]

Airborne 05.10.24: Icon Auction, Drunk MedEvac Pilot, Bell ALFA

Also: SkyReach Parts Support, Piper Service Ctr, Airliner Near-Miss, Airshow London The Judge overseeing Icon's convoluted Chapter 11 process has approved $9 million in Chapter 11 >[...]

Airborne Affordable Flyers 05.16.24: PRA Runway, Wag-Aero Sold, Young Eagles

Also: Paramotor Champ's, Electric Ultralight, ICON BK Update, Burt Rutan at Oshkosh! The Popular Rotorcraft Association is reaching out for help in rebuilding their private runway >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC