Attachment 4 and SV Stowed Diagrams (20201023 - Rev 2).pdf

PDF 2 MB Posted Oct 23, 2020

Attached to: SDA Tranche 0 Launch Services
Solicitation number: HQ085021R0001
Issued by: Space Development Agency

About this file

Written by GovTribe AI · Dec 28, 2023

This attachment to a solicitation provides specifications for twenty-eight satellite vehicles to be delivered to orbit under the Space Development Agency's Tranche 0 Launch Services procurement. The contractor shall transport ten Group A and three Group B satellites for Transport Vendor 1 with masses between 172.4-180.4kg and dimensions of 87x87x115-122cm using a 15-inch adapter. Transport Vendor 2 requirements include seven Group A satellites with masses of 199±20kg and dimensions of 107x84x124cm and three Group B satellites with masses of 180±20kg and dimensions of 107x84x140cm, both using a 24-inch adapter. Additionally, the contractor shall deliver four satellites for Tracking Vendor 1 with total masses of 2975kg for two satellites or 5111kg for four satellites stacked on an ESPA ring, and four satellites for Tracking Vendor 2 each with a mass of 249±15kg and dimensions of 153.4x106.7x133.1cm attached to an ESPA Grande ring via motorized lightbands. The first launch is required by September 2022 with all satellites to be in orbit by 31 March 2023 under the solicitation from the Space Development Agency.

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Other files

File	Type	Posted
HQ085021R0001 - Amendment 3 (10-29-20).pdf	PDF	Oct 29, 2020
HQ085021R0001 Attachment 2 - Proposal Instructions (Rev 2).pdf	PDF	Oct 23, 2020
SDA T0 Consolidated Launch Services QandA Amendment 0002 (20201023).pdf	PDF	Oct 23, 2020
HQ085021R0001 Attachment 1 - Tranche 0 Launch Services SOW (Rev 1).pdf	PDF	Oct 16, 2020
SDA T0 Launch Services Q and A (10-16-20).pdf	PDF	Oct 16, 2020
HQ085021R0001 Attachment 5 - Tranche 0 Launch Services Deliverables List (Rev 1).pdf	PDF	Oct 16, 2020
HQ085021R0001 Attachment 2 - Proposal Instructions (Rev 1).pdf	PDF	Oct 16, 2020
HQ085021R0001 Attachment 7 - SBPCD.pdf	PDF	Oct 16, 2020
HQ085021R0001 Attachment 4 - SV Planning Info (Rev 1).xlsx	XLSX spreadsheet	Oct 16, 2020
HQ085021R0001 Attachment 3 - Evaluation Factors.pdf	PDF	Oct 16, 2020
HQ085021R0001 - Amendment 1 (10-16-20).pdf	PDF	Oct 16, 2020
HQ085021R0001 Attachment 6 - Tranche 0 Launch Services Notional Payment Plan (Rev 1).pdf	PDF	Oct 16, 2020
HQ085021R0001 Attachment 5 - Tranche 0 Launch Services Deliverables List.pdf	PDF	Oct 6, 2020
HQ085021R0001 Attachment 2 - Proposal Instructions.pdf	PDF	Oct 6, 2020
HQ085021R0001 Attachment 1 - Tranche 0 Launch Services SOW.pdf	PDF	Oct 6, 2020
HQ085021R0001 Attachment 7 - SBPCD.pdf	PDF	Oct 6, 2020
HQ085021R0001 Attachment 6 - Tranche 0 Launch Services Notional Payment Plan.pdf	PDF	Oct 6, 2020
HQ085021R0001.pdf	PDF	Oct 6, 2020
HQ085021R0001 Attachment 3 - Evaluation Factors.pdf	PDF	Oct 6, 2020
HQ085021R0001 Attachment 4 - Tranche 0 Launch Services SV Planning Info.pdf	PDF	Oct 6, 2020

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Solicitation HQ085021R0001, Attachment 4

Transport Vendor 1

Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

Group A 7 172.4+/-20 87 87 115 PSC MLB MK2, RUAG PAS 381S, or equivalent

No access requirements after SV encapsulation Fuel: Solid Indium (Inert) – will arrive at the launch facility fully fueled.

Group B 3 180.4+/-20 87 87 122 PSC MLB MK2, RUAG PAS 381S, or equivalent

No access requirements after SV encapsulation Fuel: Solid Indium (Inert) – will arrive at the launch facility fully fueled.

Transport Vendor 2

Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

Group A 7 199+/-20 107 84 124

7.2 kg leave behind mass includes the following hardware elements, to be provided by the LSC:

1) 4x 4-Point HDRM (3.2 kg) is a device used to separate the SV from the LV

2) Adapter Plate (est 3.2 kg) used to interface the four HDRM separation devices to the 24" diameter ESPA port

3) Harness (est 0.8 kg) is a flight harness that interfaces the four HDRMs to the launch vehicle for separation commands

24" port desired (15" port requires heavier adapter plate)

No access requirements after SV encapsulation Fuel: Currently an open trade between inert and chemical propellant. Proposers shall list supported propellant types along with any associated proposal impacts. If the chosen propellant is inert, the SVs will arrive at the launch facility fully fueled. If the chosen propellant is chemical, it will need to be loaded at the Payload Processing Facility

(PPF).

Group B 3 180+/-20 107 84 140

7.2 kg leave behind mass includes the following hardware elements, to be provided by the LSC:

1) 4x 4-Point HDRM (3.2 kg) is a device used to separate the SV from the LV

2) Adapter Plate (est 3.2 kg) used to interface the four HDRM separation devices to the 24" diameter ESPA port

3) Harness (est 0.8 kg) is a flight harness that interfaces the four HDRMs to the launch vehicle for separation commands

24" port desired (15" port requires heavier adapter plate)

(PPF).

Tracking Vendor 1 Stowed Dimensions

No. of SVs Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

2975 kg* for 2SV launch configuration, 5111 kg* for 4SV launch configuration, *inclusive of SVs, adaptor, and SV separation hardware from adapter

SVs stacked on top of ESPA ring Separation system and adapter to be provided by Tracking Vendor 1

No access requirements after SV encapsulation;

PPF Cleanliness: Class 100,000

Fuel: Krypton gas, to be loaded at the Payload Processing Facility (PPF).

Tracking Vendor 2 Stowed Dimensions

No. of SVs Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

4 249+/-15 153.4 106.7 133.1

Current baseline would be an ESPA Grande adapter with 4 Satellites attached to the ESPA ring via 19.848" Motorized Lightband 19.848

PPF Cleanliness: Class 100,000; access requirements: visual inspection for encapsulation damage only (no personnel access)

Fuel: Green propellant (based on ADN - Ammonium DiNitrimide). Fueled prior to mating to the ESPA ring at the Payload Processing Facility (PPF)

No. of SVs LV (ESPA) Adapter Interface Stowed Dimensions

Other considerations (e.g. GN2 purge, air, etc.)

Other considerations (e.g. GN2 purge, air, etc.)No. of SVs LV (ESPA) Adapter Interface Stowed Dimensions

See provided diagrams

LV (ESPA) Adapter Interface

Fuel

Other considerations (e.g. GN2 purge, air, etc.) Fuel

SV Information

Solicitation HQ085021R0001, Attachment 4

Transport Vendor 1

No. of SVs Stowed Dimensions LV (ESPA) Adapter Interface Other considerations (e.g. GN2 purge, air, etc.) Fuel

Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

Group A 7 172.4+/-20 87 87 115 PSC MLB MK2, RUAG PAS 381S, or equivalent 15 No access requirements after SV encapsulation Fuel: Solid Indium (Inert) – will arrive at the launch facility fully fueled.

Group B 3 180.4+/-20 87 87 122 PSC MLB MK2, RUAG PAS 381S, or equivalent 15 No access requirements after SV encapsulation Fuel: Solid Indium (Inert) – will arrive at the launch facility fully fueled.

Transport Vendor 2

No. of SVs Stowed Dimensions LV (ESPA) Adapter Interface Other considerations (e.g. GN2 purge, air, etc.) Fuel

Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

Group A 7 199+/-20 107 84 124 7.2 kg leave behind mass includes the following hardware elements, to be provided by the LSC:

1) 4x 4-Point HDRM (3.2 kg) is a device used to separate the SV from the LV

2) Adapter Plate (est 3.2 kg) used to interface the four HDRM separation devices to the 24" diameter ESPA port

3) Harness (est 0.8 kg) is a flight harness that interfaces the four HDRMs to the launch vehicle for separation commands 24" port desired (15" port requires heavier adapter plate) No access requirements after SV encapsulation Fuel: Currently an open trade between inert and chemical propellant. Proposers shall list supported propellant types along with any associated proposal impacts. If the chosen propellant is inert, the SVs will arrive at the launch facility fully fueled. If the chosen propellant is chemical, it will need to be loaded at the Payload Processing Facility (PPF).

Group B 3 180+/-20 107 84 140 7.2 kg leave behind mass includes the following hardware elements, to be provided by the LSC:

1) 4x 4-Point HDRM (3.2 kg) is a device used to separate the SV from the LV

2) Adapter Plate (est 3.2 kg) used to interface the four HDRM separation devices to the 24" diameter ESPA port

Tracking Vendor 1

Stowed Dimensions LV (ESPA) Adapter Interface Other considerations (e.g. GN2 purge, air, etc.) Fuel

No. of SVs Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

4 2975 kg* for 2SV launch configuration, 5111 kg* for 4SV launch configuration, *inclusive of SVs, adaptor, and SV separation hardware from adapter See provided diagrams SVs stacked on top of ESPA ring Separation system and adapter to be provided by Tracking Vendor 1 No access requirements after SV encapsulation; PPF Cleanliness: Class 100,000 Fuel: Krypton gas, to be loaded at the Payload Processing Facility (PPF).

Tracking Vendor 2

Stowed Dimensions LV (ESPA) Adapter Interface Other considerations (e.g. GN2 purge, air, etc.) Fuel

No. of SVs Mass (kg) x (cm) y (cm) z (cm) LV (ESPA) Adapter Interface - Lightband or other? Size (inches)

4 249+/-15 153.4 106.7 133.1 Current baseline would be an ESPA Grande adapter with 4 Satellites attached to the ESPA ring via 19.848" Motorized Lightband 19.848 PPF Cleanliness: Class 100,000; access requirements: visual inspection for encapsulation damage only (no personnel access) Fuel: Green propellant (based on ADN - Ammonium DiNitrimide). Fueled prior to mating to the ESPA ring at the Payload Processing Facility (PPF)

115.0 MAX

87.0 MAX

-001 (GROUP A)

109.7

122.0 MAX

116.7

87.0 MAX

-003 (GROUP B)

+Z (SV)

CL +Z (SV)

+Z (SV)

Z=0 Z=0

+X (SV)

+Y (SV) +Y (SV)

+X (SV)

NOTES:

1 LV ADAPTER MOUNTING LOCATION. PLACEMENT SAME FOR GROUP B (FN2).

REV ZONE DESCRIPTION

00 DRAFT

1 1 4000389 PSC MLB MK2 15-INCH 3

1 -003 GROUP B SV 2

1 -001 GROUP A SV 1

-003 -001 PART NUMBER DESCRIPTION FN

P/N USED ON

A A

B B

C C

D D

SV STOWED

PARAMETERS

DO NOT SCALE DRAWING

801DRAFT

SHEET 1 OF 1

10/16/2020

UNLESS OTHERWISE SPECIFIED:

SCALE: 1:7 WEIGHT:

REVDWG. NO.

SIZE

TITLE:

MDWG-801DRAFT-00-801-01NAME DATE

COMMENTS:

RELEASED

MFG APPR.

ENG APPR.

CHECKED

DRAWN

FINISH

MATERIAL

INTERPRET GEOMETRIC

TOLERANCING PER:

DIMENSIONS ARE IN CM

TOLERANCES:

FRACTIONAL

ANGULAR: MACH BEND

TWO PLACE DECIMAL .030

THREE PLACE DECIMAL .010

BREAK SHARP EDGES .005-.030

ASME Y14.5

TRANSPORT VENDOR 1

UNLESS OTHERWISE SPECIFIED:

DIMENSIONS ARE IN INCHES

DIMENSIONS IN [ ]'S ARE IN MM

TOLERANCE ON DIMS:

± 1.0°

DECIMALS

±.030 ±.010 ±0.004

.XX

.XXX ANGULAR

MACHINE FINISH

32.283

2X 60.0°

49.0

55.0

1.25

LV ADAPTER INTERFACE

Z+

X+

42.00

33.25

14.00

X+

Y+

Z-

20X 1/4-20 UNC

(HDRM MOUNTING)

3X .567 2.467 4.307

19.772 21.150 3X 23.512 23.780

3X .267

2.629 4.007

19.472 21.312

3X 23.212

LV ADAPTER INTERFACE

X+

Y+

Z+

X+

NOTES UNLESS OTHERWISE SPECIFIED:

THIS IS A LIMITED DIMENSION DRAWING.1.

X+

Z+

Y+ Y+

BOTTOM VIEW (NORMAL TO SPACECRAFT

MOUNTING FACE (Z+))

SIDE VIEW SIDE VIEW

TOP VIEW

Y+

Z+

18 7 6 5 4 3 2

120664 -SEE NOTESFINISH

REV

SHEET 1 OF 1

PART NO:

WEIGHT:SCALE: 1:12

6J8J8

CAGE CODE

C 1098119.20

SIZE

DESCRIPTION:

14 OCT 2020

MATERIAL

DRAWN

DATEPERSONNEL

APPROVED

14 OCT 2020DESIGNED

TRANSPORT VENDOR 2

Tracking Vendor 1 – 2 SV Stacked Configuration Tracking Vendor 1 – 4 SV Stacked Configuration

Adapter Adapter2 Stacked SVs 4 Stacked SVs

Adapter connects to the 1.575m ring and will remain attached to the ring after SVs separate from adapter

Dimensions are in mm

Tracking Vendor 1 – 4 SV Stacked Configuration

Dimensions are in mm

Tracking Vendor 1 – 4 SV Stacked Configuration

Tracking Vendor 1 – 2 SV Stacked Configuration

52.4” (1331mm)

60.4” (1534mm)

38” (965mm)

TRACKING VENDOR 2

42” (1067mm)

TRACKING VENDOR 2

Attachment 4 (20201023)

Slide Number 1

SV Stowed Diagrams

SV Diagrams

Transport Vendors 1 and 2 Diagrams

120664-6_WILDFIRE_STOWED_ENVELOPE_20201014

Sheet1

Drawing View1

Drawing View2

Drawing View3

Drawing View4

Drawing View5

T0TL_RECALL_York SV_Stowed_Dimensions_DRAFT

Sheet1

Drawing View1

Drawing View2

Drawing View3

Drawing View5

Drawing View6

Drawing View7

Tracking Vendor 2 Stowed Diagram

SpaceX SV Stowed Diagrams

File details come from the government source that posted it. Updated Oct 23, 2020.