18.__CTVS_Cross_Reference_MatrixV1.pdf
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PR: FD2060‐17‐00923 Revision: 2/10/17
Attachment #: 18 RFP Number: SPRWA1‐17‐R‐0018
Cross Reference Matrix
Requirement Reference Technical Requirements
Reference (Technical Proposal)
Notes
1 Can deliver prototypes and TDP within 3 months of contract award?
RDS 4.2
2 Complete HAMAAR attached? Attachment, RDS 4.0
3 Can submit certification of satisfactory completion of safety-of-flight test?
RDS 4.4
4 CDRL A001 RDS 4.3
5 CDRL A002 RDS 4.4
6 CDRL A003 RDS 4.5, 4.7,
4.7.1, 4.7.5
7 CDRL A004 RDS 4.5
8 CDRL A005 RDS 4.6
9 CDRL A006 RDS 4.7.4
10 CDRL A007 RDS 4.10.1
11 CDRL A008 RDS 4.8.2
12 CDRL A009 RDS 4.8.4
13 3.1.2 Interface definition 3.1.2
14 3.1.2.1 Input discretes 3.1.2.1
15 3.1.2.2.1 Video output 3.1.2.2.1
16 3.1.2.3 Power Input 3.1.2.3
17 3.1.2.4 Physical interface 3.1.2.4
18 3 .1. 3 Major component list 3 .1. 3, RDS 1.2
19 3.2.1.1.1 Lens 3.2.1.1.1
20 3.2.1.1.2 Entrance pupil location 3.2.1.1.2
21 3.2.1.1.3 Filter 3.2.1.1.3
22 3.2.1.1.4 Polarization 3.2.1.1.4
23 3.2.1.1.5 Anti-aliasing 3.2.1.1.5
24 3.2.1.2 Event mark 3.2.1.2
25 3.2.1.3 Light level 3.2.1.3
26 3.2.1.4 Signal-to-noise ratio 3.2.1.4
27 3.2.1.5 Resolution 3.2.1.5
28 3.2.1.6.1 Gray shades 3.2.1.6.1
29 3.2.1.6.2 Gamma 3.2.1.6.2
30 3.2.1.6.3 Brightness transient response
3.2.1.6.3
31 3.2.1.7 Spectral response 3.2.1.7
32 3.2.1.8 Flicker and jitter 3.2.1.8
33 3.2.1.9 Brightness uniformity 3.2.1.9
34 3.2.1.10 Solar effects 3.2.1.10
34 3.2.1.11 Field-of-view (FOV) 3.2.1.11
35 3.2.1.12.1 Raster center 3.2.1.12.1
36 3.2.1.12.2 Scaling 3.2.1.12.2
37 3.2.1.12.3 Alignment coefficients 3.2.1.12.3
38 3.2.1.12.4 Distortion 3.2.1.12.4
39 3.2.1.13 Blooming 3.2.1.13
40 3.2.1.14 Blemishes 3.2.1.14
41 3.2.1.15 Service life 3.2.1.15
42 3.2.1.15.1 Operational service life 3.2.1.15.1
43 3.2.1.15.2 Storage 3.2.1.15.2
44 3.2.1.16 Electrical power characteristics
3.2.1.16
45 3.2.1.16.1 Steady-state and transient operation
3.2.1.16.1
46 3.2.1.16.2 Power requirements 3.2.1.16.2
47 3.2.1.16.3 Power interruption 3.2.1.16.3
48 3.2.1.17 Warm-up time 3.2.1.17
49 3.2.1.18 Thermal design 3.2.1.18
50 3.2.1.18.1 Cooling methods 3.2.1.18.1
51 3.2.1.18.2 Thermal analysis 3.2.1.18.2
52 3.2.2.1 Weight 3.2.2.1
53 3.2.2.2 Dimensions 3.2.2.2
54 3.2.3 Reliability 3.2.3
55 3.2.3.1 Environmental stress screening (ESS)
3.2.3.1
56 3.2.3.2 Derating criteria 3.2.3.2
57 3.2.4.2 Maintenance time 3.2.4.2
58 3. 2. 4. 2. 1 On-aircraft maintenance 3. 2. 4. 2. 1
59 3. 2. 4. 3. 1 Equipment handling 3. 2. 4. 3. 1
60 3.2.4.3.2 Aircraft ready condition 3.2.4.3.2
61 3.2.4.3.3 Adjustments 3.2.4.3.3
62 3.2.4.3.4 Reversibility restrictions 3.2.4.3.4
63 3.2.4.3.5 Labeling 3.2.4.3.5
64 3. 2. 4. 3. 6 Preventive maintenance 3. 2. 4. 3. 6
65 3.2.4.4 Maintainability Design to requirements (MDTR)
3.2.4.4
66 3.2.5.1.1 Surrounding air temperature 3.2.5.1.1
67 3.2.5.1.2 Surrounding air pressure 3.2.5.1.2
68 3.2.5.2 Windblast 3.2.5.2
69 3.2.5.3 Explosive atmosphere 3.2.5.3
70 3.2.5.4 Vibration environment 3.2.5.4
71 3.2.5.5 Mechanical shock 3.2.5.5
72 3.2.5.6.1 Limit load factors 3.2.5.6.1
73 3.2.5.6.2 Ultimate load factors 3.2.5.6.2
74 3.2.5.6.3 Crash landing load factors 3.2.5.6.3
75 3.2.5.7 Sunshine 3.2.5.7
76 3.2.6 Transportability 3.2.6
77 3.3 Design and construction 3.3
The purpose of this cross reference matrix is to show how each proposal will be evaluated. Each offeror shall complete the matrix indicating how their proposal meets all requirements and use the reference column to reference where in their proposal the information can be found. The details explanation shall describe how the offeror shall all meet of the section 3 of the specification and contract requirements.
Failure by the offeror to complete the matrix will result in the offeror being considered as failing to meet the RFP terms and conditions.
78 3.3.1 Materials, processes and parts 3.3.1
79 3.3.1.1 Electrostatic discharge (ESD) protection
3.3.1.1
80 3.3.1.1.1 Assembly level design protection
3.3.1.1.1
81 3.3.1.1.2 Equipment (LRU/module) level design protection
3.3.1.1.2
82 3.3.1.2 Finish and color 3.3.1.2
83 3.3.1.3 Conformal coatings 3.3.1.3
84 3.3.1.4 Castings 3.3.1.4
85 3.3.1.5 Soldering 3.3.1.5
86 3.3.1.6.1 Optical components 3.3.1.6.1
87 3.3.1.6.2 Coating characteristics 3.3.1.6.2
88 3.3.2.1 General 3.3.2.1
89 3.3.2.2 EMI safety-of-flight (SOF) test requirements
3.3.2.2
90 3.3.2.3 EMI filters 3.3.2.3
91 3.3.2.4 Installation/ integration requirements
3.3.2.4
92 3.3.2.5 Electrical bonding requirements
3.3.2.5
93 3.3.2.6 Grounding 3.3.2.6
94 3.3.2.7 Shielding 3.3.2.7
95 3.3.3.1 Marking of parts and assemblies
3.3.3.1
96 3.3.3.2 Identification of units 3.3.3.2
97 3.3.3.3 Alignment coefficients label 3.3.3.3
98 3.3.4 Workmanship 3.3.4
99 3.3.5 Interchangeability 3.3.5
100 3.3.6.1 Toxicity 3.3.6.1
101 3.3.6.2 Electronic equipment hazards
3.3.6.2
102 3.3.6.3 Personnel hazards and safety
3.3.6.3
103 3.3.6.5 Ozone depleting chemicals 3.3.6.5
104 3.3.7 Human performance/ human engineering
3.3.7
105 3.3.8 Switching transient 3.3.8
106 3.5 Logistics 3.5
107 3.5.1 Maintenance 3.5.1
108 3.5.2 Supply 3.5.2
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