ONIR Industry Day Slides.pdf

NATIONAL NUCLEAR

SECURITY ADMINSTRATION

OFFICE OF NUCLEAR

INCIDENT RESPONSE (NA-

84) INDUSTRY DAY

October 29, 2019

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This Industry Day is:

• For information and planning purposes.

• No solicitation exists at this time.

• No decision has been made to initiate a future acquisition.

• The information from this event today will not be considered as an obligation by the Government.

Agenda

GENERAL SESSION

(9 AM to 12 NOON)

Opening Remarks

Logistics and Administrative Topics

Overview/Physical review of helicopter

Written Question Collection

Q&A Session

BREAK

(12 NOON to 1 PM)

INTERVIEW SESSION

(1 PM to 4 PM)

One-on-One Interviews

OPENING REMARKS

Les Winfield, Nevada Field Office (NFO) Aviation Manager

Yolanda Robinson-Freeman, Contracting Officer, NNSA

Background

■ The Office of Nuclear Incident Response (ONIR) is the premier technical leader in responding to and successfully resolving nuclear and radiological incidents or accidents.

■ Technical teams are prepared to search for radioactive material and help manage the consequences of a release of radioactive material into the environment.

■ National Nuclear Security Administration (NNSA) Aerial Measuring System (AMS) has specialized airborne radiation detection systems to provide real-time measurements of low levels of air and ground contamination.

■ The aircraft operations are at Joint Base Andrews, MD, and Nellis Air Force Base, Las Vegas, NV.

Requirements

■ Survey Flight Envelopes: 50-3,000 feet above ground level (AGL), from 60-80 knots ground speed

■ Crew: Two pilots, two technical specialists, two observers

■ Flight Patterns: Predominantly parallel line patterns with precise, narrow offset distances and consistent AGL altitudes (often performed over congested areas of the country)

Minimum Requirements

1. Newly manufactured, twin-turbine engine powered rotary wing aircraft

2. 14 CFR Part 91 General Operating and Flight Rules Compliant

3. FAA Type Certificate

4. FAA Airworthiness Certificate

5. Certified Category A

6. Performance Class 1 or 2 Operations

7. Mission Availability Rate 95% (24-hour/365-day Emergency Response)

8. Temperature operating range from - 40 to +45 degrees C

9. Day and night operations

10. Certified Single Pilot Operations

11. All-Weather Operations

12. Certification for flight into known icing conditions (§ 29.1419 Ice protection), or Ice protection systems for aircraft engines, airframe, and airframe components

13. Certified for Visual Flight Rules

(VFR)

14. Certified for Instrument Flight Rules

(IFR)

15. Cargo hook

16. Dual flight controls

17. Capable of carrying 1700 lbs. of detectors and mission equipment

18. Capable of mounting the following detector equipment on the aircraft:

Quantity Detector Length (Inches)

Width (Inches)

Height (Inches)

Total Area Sq. Ft.

Total Weight Pounds

4 RSX-3 29.75 16.25 7 13.4 400

2 HPGe 14.5 6.5 14.5 1.3 46 1 N0 79.5 18.25 8.75 10.1 230

Minimum Requirements

19. Detector mounting provisions and restrictions are:

– Equipment is not stacked

– Equipment has minimal aircraft structure between it and the ground

– Equipment is not mounted over a variable volume fuel tank

20. Seating provisions for two pilots, two technicians, and two observers.

21. Mission endurance with mission equipment, detectors, and personnel > 3 hours flight time

22. 2K volt-amps available for mission equipment

23. Hover in ground effect ceiling, ISA, at max gross takeoff weight, 15,000 feet

24. Detector and mission equipment volume > 65 cu ft.

25. Avionics output to mission equipment

– Radar/Laser Altimeter

– Heading and Speed

– 3-D Orientation

26. Onboard Wi-Fi

27. SATCOM – voice and data

28. Air-to-ground communications

29. Wire strike protection system

30. Air conditioning/Heat for cockpit and cabin

31. ADSB In/Out

32. TCAS II Traffic Collision Avoidance System

33. Helicopter Terrain Avoidance System (HTAWS)

34. Weather Radar

35. Fully-Integrated Flight Management System (FMS)

36. Distance Measruing Equipment

(DME)

37. ICS/Communication System with wired jacks and headsets with cabin/cockpit isolation

Additional Features – Air Frame

■ Active Vibration Management System

■ Energy Absorbent Self- Sealing Fuel Tanks

■ Crash-Worthy Seating Arrangement

■ Energy-Absorbing Seats

■ Energy-Absorbing Landing Gear

■ Fuselage and Rotor System Bird Strike Protection

■ Main Engine Turbine Burst Protection

■ Automatic Deployable Emergency Locator Transmitter (ADELT)

■ Crashworthy Fuselage

■ Designated Operator Seats for Two Crew Including Console

■ Mounting Points for Mission Equipment (e.g.

detectors, cameras, LIDAR, etc.)

■ Lightning Protection

■ High Intensity Radiated Field (HIRF) Protection

■ Gimbal Mount and/or Optical Port

■ Auxiliary Power Unit (APU)

■ Downward-Facing Illumination and Navigation Lighting Fixtures

Additional Features- Mission Equipment Electrical Power

■ Mission Inverter (separate from aircraft-required power)

■ 110 VAC power outlets in cockpit and cabin

■ 28 VDC power for mission equipment in cabin

■ USB charge ports in cockpit and cabin

■ Integrated battery UPS capable of mission equipment ground operations for 45 minutes

Additional Features – Cockpit

■ Full Glass Cockpit

■ Integrated Flight Display

System

■ Center Multi-Function

Display

■ Digital Moving Map

■ Enhanced Ground

Proximity Warning System

(EGPWS)

■ Laser Obstacle Avoidance System (LOAM)

■ Second DME

■ Second FMS

■ Search and Rescue

Patterns in FMS

■ Automatic Identification

System

■ Redundant Full Authority

Digital Engine Control (FADEC) System

■ Backup System In The Event Of Both FADEC Systems Fail

■ Onboard Health and Usage Monitoring System (HUMS)

■ Digital Autopilot (4 Axis)

■ Automated Flight Control

System (AFCS) With Auto- Hover

■ Automated Flight Control System (AFCS) With Flight to Geographic Point Capability

■ Flyable With All Automatic Systems Disabled

Additional Features - Operations

■ Broadband

■ Air-to-Ground Communications

■ Initiating Startup Sequence to Ready-For-Takeoff Time

■ Forward Looking Infrared (FLIR)

■ Laser Altimeter

■ Radar Altimeter Avionics Output To Detection Equipment

■ Laser Altimeter Avionics Output To Detection Equipment

■ Heading & Speed Avionics Output To Detection Equipment

■ 3-D Orientation Avionics Output To Detection Equipment

Document Submission

Submit electronic files via email at jeff.sena@nnsa.doe.gov, at 4:00 p.m., MT, November 6, 2019.

■ Technical Capability Statement and Pricing Information.

– Limited to 20 pages (includes cover page and index).

– Single-sided, single-spaced, Times New Roman 12 pt. font, 1 inch margins.

■ Company Profile.

– Limited to 5 pages.

– Provide the size of the business (large or small).

– Small business firms must identify socioeconomic categories:

– Including (not limited to): 8(a) Business Development Program, Small Disadvantage Business, HUBZone, Service-Disabled Veteran-Owned, Woman- Owned Small Business concerns.

Moving Forward

■ Results of this information will be used to determine potential levels of competition available in the industry, and establish an acquisition strategy, whether full and open competition or small business set-aside.

■ For future announcements, the solicitation documents, and any drafts will be posted on the Federal Business Opportunities (FBO) website, www.fbo.gov. It is the responsibility of all potential offerors to monitor the FBO website for any amendments, updates, or responses to questions and answers.

■ Questions? Direct to Jeff Sena, Contract Specialist, jeff.sena@nnsa.doe.gov mailto:jeff.sena@nnsa.doe.gov

QUESTIONS?