Attachment B - Figures.pdf
PDF 9 MB Posted
- Attached to
- Multi-Hoist Winch System & Air Caster System Federal contract opportunity
- Solicitation number
- 80LARC858109Q
About this file
This document is an attachment containing figures for a Statement of Work related to a federal contract solicitation for a Multi-Hoist Winch System and Air Caster System procurement at the NASA Langley Research Center Landing and Impact Research Facility.
The solicitation is a Request for Quotation (RFQ) under number 80LARC858109Q, with key deadlines of February 27, 2024 for site visit requests, March 15, 2024 for questions, and April 2, 2024 for quotation submissions. The contract requires delivery of various winches, an air caster system, power drives, cables, sheaves, controls, and drawings by November 1, 2024. This is a 100% small business set-aside under NAICS code 333923. The award will be based on technical capability, price, and delivery. Potential offerors are encouraged to attend an optional site visit on March 8, 2024.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Update01 - Figure20 High Resolution.pdf | ||
| Attachment A - SOW.pdf | ||
| Attachment E - Offeror Questions.pdf | ||
| Attachment A - SOW.pdf | ||
| Attachment C - Additional Terms and Conditions.pdf | ||
| Attachment D - Site Visit Instructions.pdf | ||
| Attachment B - Figures.pdf | ||
| Attachment A - SOW.pdf |
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Text version
Attachment B
80LARC858109Q
ATTACHMENT FOR STATEMENT OF WORK
for Multi-Hoist System and Air Caster System Procurement for the NASA Langley Research Center Landing and Impact Research Facility
List of Figures:
Figure 1: Photo of Landing and Impact Research Facility (LandIR) with labels for the Gantry Figure 2: Photo of Gantry Center Bent (Side View) Figure 3: Photo of Gantry Center Bent (Bottom View) Figure 4: Photo of Gantry Center Bent (Top View Looking North) Figure 5: Photo showing examples of previous Crane Operations at the Gantry 3/20/24 Update - Figure 6: Initial Vertical Lift of the Lander at the Gantry (Side View) 3/20/24 Update - Figure 7: Lander shown at Peak Pullback for Impact Dynamics Test at the Gantry (Side View) 3/20/24 Update - Figure 8: Lander shown at Peak Pullback for Impact Dynamics Test at the Gantry (Perspective View) 3/20/24 Update - Figure 9: Upper and Lower Platform Installation on Gantry Center Bent 3/20/24 Update - Figure 10: Upper Platform Design (Approx. 100ft long x 15ft wide x 6ft high) 3/20/24 Update - Figure 11: Upper Platform Design (Top & Side View) 3/20/24 Update - Figure 12: Lower Platform Design (Approx. 4ft wide x 15ft long & Approx. 3k lbs.)
3/20/24 Update - Figure 13: Ground Tower Design (Approx. 11ft wide x 23ft long x 30ft tall) Figure 14: Ground Towers 1 & 2 Positioned at Gantry Center Bent Leg (Perspective View) Figure 15: Ground Tower Position at Gantry Center Bent Leg (Side View) 3/20/24 Update - Figure 16: Impact Barrier Design Figure 17: Assembly Design with Lander on Concrete at Initial Vertical Lift Position (Side View) Figure 18: Assembly Design with Lander on Impact Barrier (Side View) Figure 19: Assembly Design with Lander on Impact Barrier (Perspective View) NEW - Figure 20: Impact Barrier to Air Bearing Interface Control Document
Figure 1: Photo of Landing and Impact Research Facility (LandIR) with labels for the Gantry
Figure 2: Photo of Gantry Center Bent (Side View)
Figure 3: Photo of Gantry Center Bent (Bottom View)
Figure 4: Photo of Gantry Center Bent (Top View Looking North)
Figure 5: Photo showing examples of previous Crane Operations at the Gantry
(Removed) Figure 6: Initial Vertical Lift of the Lander at the Gantry (Side View)
Updated To:
Figure 6: Initial Vertical Lift of the Lander at the Gantry (Side View)
(Removed) Figure 7: Lander shown at Peak Pullback for Impact Dynamics Test at the Gantry (Side View)
Figure 7: Lander shown at Peak Pullback for Impact Dynamics Test at the Gantry (Side View)
(Removed) Figure 8: Lander shown at Peak Pullback for Impact Dynamics Test at the Gantry (Perspective View)
Figure 8: Lander shown at Peak Pullback for Impact Dynamics Test at the Gantry (Perspective View)
(Removed) Figure 9: Upper and Lower Platform Installation on Gantry Center Bent
Figure 9: Upper and Lower Platform Installation on Gantry Center Bent
(Removed) Figure 10: Upper Platform Design (Approx. 70ft long x 14ft wide x 2ft high & 57k-67k lbs.)
Figure 10: Upper Platform Design (Approx. 100ft long x 15ft wide x 6ft high)
(Removed) Figure 11: Upper Platform 60k lbs. Capacity Winch Double Sheaves (right) & Swing Cable Sheave (left
Update To:
Figure 11: Upper Platform Design (Top & Side View)
(Removed) Figure 12: Lower Platform Design (Approx. 4ft wide x 14ft long & Approx. 11k lbs.)
Figure 12: Lower Platform Design (Approx. 4ft wide x 15ft long & Approx. 3k lbs.)
(Removed) Figure 13: Ground Tower Design (Approx. 10ft wide x 23ft long x 30ft tall)
Figure 13: Ground Tower Design (Approx. 11ft wide x 23ft long x 30ft tall)
Figure 14: Ground Towers 1 & 2 Positioned at Gantry Center Bent Leg (Perspective View)
Figure 15: Ground Tower Position at Gantry Center Bent Leg (Side View)
(Removed) Figure 16: Impact Barrier Design
Figure 16: Impact Barrier Design
Figure 17: Assembly Design with Lander on Concrete at Initial Vertical Lift Position (Side View)
Figure 18: Assembly Design with Lander on Impact Barrier (Side View)
Figure 19: Assembly Design with Lander on Impact Barrier (Perspective View)
Figure 20: Impact Barrier to Air Bearing Interface Control Document
File details come from the government source that posted it. Updated .