SOLICITATION NOTICE
A -- Liquid Apogee Engine (LAE) Propulsion Capability Study - Presolicitation Notice of Contract Award
- Notice Date
- 9/19/2019
- Notice Type
- Presolicitation
- NAICS
- 336415
— Guided Missile and Space Vehicle Propulsion Unit and Propulsion Unit Parts Manufacturing
- Contracting Office
- Department of the Air Force, Air Force Space Command, SMC - Space and Missile Systems Center, 483 North Aviation Blvd, El Segundo, California, 90245-2808
- ZIP Code
- 90245-2808
- Solicitation Number
- FA8808-19-R-0004
- Archive Date
- 10/19/2019
- Point of Contact
- Isabel Shvartsman, , Stacey Neyses,
- E-Mail Address
-
isabel.shvartsman@us.af.mil, stacey.neyses@us.af.mil
(isabel.shvartsman@us.af.mil, stacey.neyses@us.af.mil)
- Small Business Set-Aside
- N/A
- Description
- LAE REDACTED JUSTIFICATION AND APPROVAL In accordance with (IAW) FAR 5.201 and 5.203(a), this is a Pre-Solicitation notice for a proposed contract action where the Government intends to solicit and negotiate with only one source. IAW FAR 5.207(c)(16), any responsible sources may submit a capability statement or proposal which shall be considered by the agency. In accordance with (IAW) FAR 6.302-1(a)(2)(iii)(A-B), the Department of the Air Force, Space and Missile Systems Center (SMC), Space Development Contracting branch (SMC/DCK), located at Los Angeles AFB, CA, intends to award a new sole source contract to Aerojet Rocketdyne (Redmond, WA 98052). IAW DFARS PGI 206.302-1(d), a request for information notice for this requirement was previously posted on FBO on 10 April 2019. A copy of the Justification & Approval (J&A) is attached to this FBO notice. This effort is for engineering services, regarding the research and development of the 100-lbf LAE up to a qualification test report to verify Government 100-lbf LAE requirements. As a result of the negotiated sole source contract, the LAE effort will include the following minimum capabilities: 1.Domestic Vendor 2.100-lbf (440N) of thrust 3.Using hydrazine fuel and NTO oxidizer 4.Specific impulse >320 seconds 5.Total qualified lifetime of 9 hrs of firing time in a vacuum environment (number already includes margin) 6.Capable of implementation on any prime contractor's bus (Boeing, LM, NGIS). This affects environmental capability including shock and vibration. This also affects the range of inlet pressures that the unit must operate across. 7.Capable of operation at propellant/hardware temperatures up to 51°C (minimum) / 61°C (goal). Note that these temperatures include uncertainty and qualification margin so that implementation in a satellite design has flight capability to 30°C min / 40°C goal. 8.Qualification testing complete within 2 years to provide a mature LAE platform for future space platforms and funding constraints. Projected Request-for-Proposal (RFP) release date for this requirement is estimated to be no sooner than 15 calendar days after this Pre-Solicitation notice is posted, and will be directed solely to the prospective source identified. This notice expires 15 days after publication.
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/USAF/AFSC/SMCSMSC/FA8808-19-R-0004/listing.html)
- Place of Performance
- Address: Space and Missiles Systems Center, 483 North Aviation Blvd, El Segundo, California, 90245-2808, United States
- Zip Code: 90245-2808
- Zip Code: 90245-2808
- Record
- SN05450766-W 20190921/190919230818-e39f94c5bebe568b14c0f4364e9106a3 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
| FSG Index | This Issue's Index | Today's FBO Daily Index Page |