Analytical Services, Inc.

Al
Huntsville, AL 35806
http://www.asi-hsv.com
389 Employees

SBIR Award Summary

Total Number of Awards 21
Total Value of Awards $7.55MM
First Award Date 08/11/00
Most Recent Award Date 09/12/14

Key Personnel

Last Name Name Awards Contact
Jess Mr. Larry Jess 2 Message
Boisjolie Darren Boisjolie 1 Message
Tuder Irma Tuder 1 Message
Guthrie Dr. Mike Guthrie 4 Message
Sims Joe Sims 8 Message
Sims Joseph Sims 5 Message
Austin Jared Austin 1 Message
Fossett Sandra Fossett 2 Message
Forton Melissa Forton 1 Message
Forton Melisa Forton 0 Message
Foset Sandra Foset 0 Message

21 Awards Won

Phase 2 SBIR

Agency: Missile Defense Agency
Topic: MDA12-022
Budget: 09/12/14 - 09/09/16

Analytical Services, Inc., is pleased to present this proposal for a lightweight, low cost, high area ratio extendible nozzle design that will provide significant increases in solid divert and attitude control system (SDACS) divert performance. We propose to use a combination of low cost, lightweight refractory materials formed, using selective...

Phase 1 SBIR

Agency: Missile Defense Agency
Topic: MDA12-022
Budget: 02/25/13 - 08/25/13

ASI is pleased to team with ATK to present a novel concept for enabling large nozzle area ratio increases for future solid divert and attitude control system (SDACS) valves/thrusters. The proposed effort will demonstrate feasibility of this advanced concept through a thorough design study that includes mechanical layout and packaging, computati...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 12-1-H2.02
Budget: 01/01/13 - 12/31/13

The goal of the proposed effort is to demonstrate feasibility of using selective laser melting (SLM, an emerging manufacturing technique) to manufacture a subscale combustion chamber liner that features an advanced regenerative cooling technique that combines high performance with low pressure drop. SLM enables the ability to "print" the advanc...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 12-1-S4.03
Budget: 01/01/13 - 12/31/13

A small Mars (or other celestial body) ascent vehicle is unlikely to achieve the necessary propellant fraction required to achieve orbit. Scaling down of liquid propulsion systems, as shown in the figure, is difficult. In the 100-kg class of vehicles, liquid propellant vehicle designers should expect a propellant fraction of only 0.75. In con...

Phase 1 SBIR

Agency: National Aeronautics and Space Administration
Topic: 11-1-S5.04
Budget: 01/01/12 - 12/31/12

The long-term goal for this effort is to develop a low-cost, high-temperature thruster. Within the attitude control propulsion community, many efforts have focused on development of ultra-high temperature precious metal alloys and systems that give long life and good performance (e.g., Ir/Re). Those designs are driven by the desire to operate ...

Phase 1 SBIR

Agency: Air Force
Topic: AF112-178
Budget: 12/01/11 - 09/02/12

ABSTRACT: In the proposed effort, ASI will demonstrate the feasibility of a practical, proven method for significantly increasing the heat transfer coefficient inside regenerative cooling channels. The technique, used in the electronics industry for high heat flux removal applications, requires one additional manufacturing step and a small chan...

Phase 2 SBIR

Agency: Air Force
Topic: AF093-079
Budget: 09/21/11 - 12/20/13
PI: Joe Sims

ABSTRACT: In our proposed Phase II effort, we will be demonstrating long-lived aqueous aluminum heat pipes. The work will directly demonstrate the corrosion inhibition character of two different aqueous work fluids and the long-term heat flux performance of our heat pipe designs at an operating temperature of 200 Deg C. In addition, we will de...

Phase 1 SBIR

Agency: Missile Defense Agency
Topic: MDA10-021
Budget: 05/31/11 - 11/30/11

BMDS components must function reliably when exposed to radiation, including both nuclear weapon and natural space environments. Current tools will not allow correct evaluations of system performance. Since the current radiation environment tools were not designed to handle sub-orbital trajectories, environments have been calculated by interpolat...

Phase 2 SBIR

Agency: Navy
Topic: N092-109
Budget: 04/25/11 - 07/27/12
PI: Joe Sims

In the proposed effort, ASI will be teaming with a major propulsion contractor to develop next generation thermal stabilizers for double base propellants. The scope includes chemical synthesis, propellant development and testing, and accelerated aging.

Phase 2 SBIR

Agency: Air Force
Topic: AF083-115
Budget: 02/16/11 - 05/16/13
PI: Joe Sims

ABSTRACT: When a solid rocket motor propellant grain contains one or more flaws (cracks, debonds, casting voids) or develops them as it ages, the risks of testing that motor is significantly increased. The responsible authority must decide between testing a motor that may destroy expensive testing infrastructure and relegating a motor for demil...

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