SATPC0033946 Tab 04 4 SOW_Revised.pdf

STATEMENT OF WORK

1. Objective/Requirements NASA WSTF’s Propulsion Test Office processes, stores, and tests orbital maneuvering engines. These engines use toxic hypergolic propellants. WSTF requires a storage container/area to process, configure, stage and store engines both pre and posttest. This document outlines the requirements for the storage containers.

2. Specifications

• Two 40-foot cargo containers shall be provided. Configuration of the containers is outline in this document and in the Daigram A below

• Each cargo container shall be single use. Proof of single use containers should be available upon request.

• Each container shall be 8’x40’x9’6 with at least 1-1/8” thick wood cargo flooring

• One side of each container shall be cut open to allow the two containers to be placed next to each other (see Daigram A below

• The opening shall be reinforced with HSS 2x2x3/16 side columns, two HSS

4x2x3/16 intermediate columns, and a HSS 4x2x3/16 continuous span header tube across the top.

• Provision for reinforcing plate on the bottom rails shall be provided

• The roof seam shall include a 3-inch steel curb, polymer joint sealant caulk & foam backer, and galvanized steel ridge cap flashing to be installed onsite by WSTF personnel

• Four bridge fittings for securing the containers shall be provided

• Threshold sealant shall be provided for completing the interior joint.

• Galvanized metal threshold shall be provided to cover the floor joint between the two containers

• On one side of the enclosure an 8x8 Steel Double door with left side latch and right-side deadbolt and handle shall be installed (see Daigram A below)

• On the opposite side one commercial exterior 3068 steel personnel door with panic bar and locking latch shall be installed (see Daigram A below)

• Four 36" x 36" vinyl framed double pane window; single hung (lower half lifts to open) with removable screen mounted to 2" x 2" welded steel tube frame, no burglar bars, shall be installed. Two windows per side (see Daigram A below)

• 1’ R-6.5 closed-cell spray-applied polyurethane foam insulation shall be installed on the underneath of each cargo container floor

• 3” R-18 closed cell spray-applied polyurethane foam insulation shall be applied to the walls and ceiling.

• Oil-based epoxy coating suitable for wood or steel with anti-skid epoxy grit additive shall be applied to the floor.

• Two exterior outdoor electrical boxes with 125A capacity 4 -space panel with 60A 2 pole breaker service disconnect shall be installed. (see Daigram A below for breaker box location)

• Two interior 125A capacity 12-space panel, including 4’ LED light fixtures, and one duplex GFI outlet shall be installed.

• Four 110V duplex 20A/110V NEMA 5-20R outlets shall be installed

• Two white outdoor oval bulkhead wall light 5"W x 4-1/2"D x 8-1/2" H shall be installed. One light installed over each door entrance.

• Exterior of each container shall be painted light grey. Service life of the exterior paint shall be no less than 5 years.

• Containers shall be delivered to WSTF on a flatbed trailer. Notification prior to shipping shall be provided.

• WSTF shall provide a crane and certified heavy lift operators to unload the containers

• WSTF shall be responsible for moving and final assembling of the containers once offloaded.

• Vendor shall have at least 20 years of experience

• Vendor shall supply Safety Data Sheets (SDS’s) for materials used in construction.

• WSTF personnel shall evaluate and approve all material for compatibility with hypergolic propellant. Bids submitted without SDS’s or that use noncompatible material will be rejected.

3. Place of Performance

NASA WSTF Propulsion Test Office, 12600, NASA Road, Las Cruces, NM

4. Period of Performance Jan 22, 2024 through March 23, 2024.

Daigram A