Attachment B - Notional Test Matrix.pdf

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Learjet Acoustic Test using CJ610 engines to assess flyover noise levels
Solicitation number
80GRC021Q0006
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This document is a combined synopsis and solicitation from the National Aeronautics and Space Administration Glenn Research Center seeking offers for acoustic testing services using Learjet aircraft with CJ610 engines. Offerors are requested to conduct flyover noise testing to assess noise levels. The testing will involve four test sorties following the notional test matrices provided in an attachment. Offers are due by April 2, 2021 and shall be submitted to the contracting officer. The acquisition is set aside for small businesses. The successful offeror will be selected based on price and technical factors. Responses must comply with standard commercial items solicitation requirements and include representations and certifications.

The testing requires using Learjet aircraft equipped with CJ610 engines to collect noise data from four test sorties following the parameters in the attached matrix. Offerors must submit pricing, delivery schedule, and other standard commercial items offer information to the NASA Glenn Research Center contracting officer by April 2, 2021.

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Other files

File Type Posted
Attachment A - Learjet Acoustic Test Requirements and SOW Revised.pdf PDF
Questions and Answers.pdf PDF
Attachment C - POS Data Sheet.pdf PDF
Request for Quotation (RFQ).pdf PDF
Attachment E - DRAFT NASA-STD-7900.pdf PDF
Attachment A - Learjet Acoustic Test Requirements and SOW.pdf PDF
Attachment F - Compliance Evaluation Document - NASA-STD-7900.pdf PDF
Attachment D - POS User Manual.pdf PDF

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Notional Test Matrix Sortie 1

Run Time Description Flaps Speed 1 ~6:30 AM 1.5 EPR TBD Between Mach .2 and Mach .3

2 TBD 1.5 EPR TBD Between Mach .2 and Mach .3

3 TBD 1.5 EPR TBD Between Mach .2 and Mach .3

4 TBD 1.5 EPR TBD Between Mach .2 and Mach .3

5 TBD 1.5 EPR TBD Between Mach .2 and Mach .3

6 TBD 1.5 EPR TBD Between Mach .2 and Mach .3

7 TBD 1.6 EPR TBD Between Mach .2 and Mach .3

8 TBD 1.6 EPR TBD Between Mach .2 and Mach .3

9 TBD 1.6 EPR TBD Between Mach .2 and Mach .3

10 TBD 1.6 EPR TBD Between Mach .2 and Mach .3

11 TBD 1.6 EPR TBD Between Mach .2 and Mach .3

12 TBD 1.6 EPR TBD Between Mach .2 and Mach .3

13 TBD 1.7 EPR TBD Between Mach .2 and Mach .3

14 TBD 1.7 EPR TBD Between Mach .2 and Mach .3

15 TBD 1.7 EPR TBD Between Mach .2 and Mach .3

16 TBD 1.7 EPR TBD Between Mach .2 and Mach .3

17 TBD 1.7 EPR TBD Between Mach .2 and Mach .3

18 TBD 1.7 EPR TBD Between Mach .2 and Mach .3

Sortie 2

Run Time Description Flaps Speed 1 TBD 1.8 EPR TBD Between Mach .2 and Mach .3

2 TBD 1.8 EPR TBD Between Mach .2 and Mach .3

3 TBD 1.8 EPR TBD Between Mach .2 and Mach .3

4 TBD 1.8 EPR TBD Between Mach .2 and Mach .3

5 TBD 1.8 EPR TBD Between Mach .2 and Mach .3

6 TBD 1.8 EPR TBD Between Mach .2 and Mach .3

7 TBD 1.9 EPR TBD Between Mach .2 and Mach .3

8 TBD 1.9 EPR TBD Between Mach .2 and Mach .3

9 TBD 1.9 EPR TBD Between Mach .2 and Mach .3

10 TBD 1.9 EPR TBD Between Mach .2 and Mach .3

11 TBD 1.9 EPR TBD Between Mach .2 and Mach .3

12 TBD 1.9 EPR TBD Between Mach .2 and Mach .3

13 TBD 2.0 EPR TBD Between Mach .2 and Mach .3

14 TBD 2.0 EPR TBD Between Mach .2 and Mach .3

15 TBD 2.0 EPR TBD Between Mach .2 and Mach .3

16 TBD 2.0 EPR TBD Between Mach .2 and Mach .3

17 TBD 2.0 EPR TBD Between Mach .2 and Mach .3

18 TBD 2.0 EPR TBD Between Mach .2 and Mach .3

Sortie 3 – Repeat Sortie 1

Sortie 4 – Repeat Sortie 2

File details come from the government source that posted it. Updated .